sunday - 21st international space plane and hypersonic...

SundaySunday, 5 March 20171-NW-1 1800 - 1930 hrs

Welcome Reception Exhibit Hall

MondayMonday, 6 March 20172-PLNRY-1 0800 - 0830 hrs

Welcome Address Conference Hall

Adam SiebenhaarMach 7H Consulting

Yancheng YouXiamen University

Monday, 6 March 20173-PLNRY-2 0830 - 0900 hrs

Host Speeches Conference Hall

Daiming FanChina Academy of Engineering

Chongshi ZhuXiamen University


Keynote I: Prospective for the Next Generation of Hypersonic Education and Research: XMU Aspects Conference Hall

Session Chair: Yancheng You, Xiamen University Zeyong Yin

Xiamen University


Keynote II: Recent Advances in Hypersonic Research - A Brief Overview of China Contributed Papers Conference Hall

Session Chair: Adam Siebenhaar, Mach 7H Consulting Yancheng You

Xiamen University

Monday, 6 March 20176-NW-2 1030 - 1100 hrs

Monday Morning Coffee Break Exhibit Hall


Global Reports I Conference Hall

Moderator: Adam Siebenhaar, Mach 7H Consulting Speakers:

ChinaLihong Chen

Chinese Academy of Science

AustraliaVincent Wheatley

University of Queensland

Session Chair: Yancheng You, Xiamen University

Monday, 6 March 20178-LUNCH-1 1200 - 1330 hrs

Monday Lunch Yifu Restaurant


Global Reports II Conference Hall

Moderator: Adam Siebenhaar, Mach 7H Consulting Speakers:

BrazilJoão Martos

Aeronautics Institute of Technology – ITA

EuropeJohan SteelantESA-ESTEC/NL

JapanMasataka Maita

International Aerospace Consulting

RussiaSergey Chernyshev

TsAGI

United StatesThomas Jackson

Air Force Research Laboratory


Monday Afternoon Coffee Break Exhibit Hall

Monday, 6 March 201711-LEC-1 1630 - 1730 hrs

Culpepper Lecture: Some Progresses of High Speed Air Breathing Research in CARDC Conference Hall

Session Chair: Adam Siebenhaar, Mach 7H Consulting Jialing Le

China Aerodynamic Research and Development Center


Monday Evening Coffee Break Conference Hall


Monday Evening Concert Concert Hall

TuesdayTuesday, 7 March 201714-SB-1 0730 - 0800 hrs

Tuesday Morning Speakers’ Briefing Session Rooms

Tuesday, 7 March 201715-HYTASP-1 Computational Methods I Conference Room 1Chaired by: V. WARTEMANN, German Aerospace Center and M. SUN, National University of Defense Technology0800 hrsAIAA-2017-2100Mass-Driver- and SCRamjet-Assisted Surface-to-Orbit Modeling and SimulationM. Wittal, J. Benavides, Embry-Riddle Aeronautical University, Prescott, AZ

0830 hrsAIAA-2017-2101The Influence of Reynolds Stress on the Laminar Heat Transfer Characteristics of Hydrocarbon FuelR. Zhang, S. Zheng, J. Le, China Aerodynamics Research and Development Center, Mianyang, China

0900 hrsAIAA-2017-2102The Vision-based Relative Navigation Using Improved Adaptive Cubature Huber-based FilteringX. Zhang, N. Cui, X. Wang, H. Cui, Harbin Institute of Technology, Harbin, China

0930 hrsAIAA-2017-2103Development and Validation of a Conjugate Heat Transfer Code for Regenerative Cooling Structure with OpenFOAMH. Pu, S. Li, M. Dong, S. Jiao, Y. Shang, Dalian University of Technology, Dalian, China

Tuesday, 7 March 201716-HYTASP-2 Hypersonic Fundamentals and History I Conference Room 7Chaired by: M. SMART, The University of Queensland and J. REN, Tsinghua University0800 hrsAIAA-2017-2104Experimental study of unsteady oblique shock train and boundary layer interactionsC. Cheng, C. Wang, K. Cheng, Y. Jiao, Nanjing University of Aeronautics and Astronautics, Nanjing, China

0830 hrsAIAA-2017-2105The Research on the Nonlinear Coupling Problem of Aerodynamics/Structure/Propulsion for Air-breathing VehicleC. Bing, C. Gong, L. Gu, S. Tang, Northwestern Polytechnical University, Xi’an, China

0900 hrsAIAA-2017-2106Aeroelastic Analysis for Response Prediction of Hypersonic Vehicle RudderL. Huo, T. Yang , National University of Defense Technology, Changsha, China

Tuesday, 7 March 201717-HYTASP-3 Missions and Vehicles I Conference Room 4Chaired by: A. PROKHOROV, Central Institute of Aviation Motors (CIAM) and G. LI, University of Electronic Science and Technology of China0800 hrsAIAA-2017-2107Trajectory Design of a Rocket-Scramjet-Rocket Multi-Stage Launch SystemS. Forbes-Spyratos, M. Kearney, M. Smart, I. Jahn, University of Queensland, Brisbane, Australia

0830 hrsAIAA-2017-2108United Trajectory Design Method for Return to Launch Site of Suborbital Reusable Launch VehicleQ. Hao, S. Peng, L. Xinguo, Northwestern Polytechnical University, Xi’an, China

0900 hrsAIAA-2017-2109An Improved Predictor-corrector Reentry Guidance for Low L/D SpacecraftE. Yong, G. Li, K. Qin, University of Electronic Science and Technology of China, Chengdu, China

0930 hrsAIAA-2017-2110Investigation of a Wide Range Adaptable Hypersonic Dual-Waverider Integrative Design Method Based on Two Different Types of 3D Inward-Turning InletsX. Xianhong, L. Yuan, Z. Qian, Aviation Industry Corporation of China (AVIC), Shenyang, China

Tuesday, 7 March 201718-HYTASP-4 Power and Control Systems I Conference Room 5Chaired by: K. KREMEYER, Physics, Materials, and Applied Mathematics Research, LLC and H. YAN, Northwestern Polytechnical University0800 hrsAIAA-2017-2111Design of Lateral Control System for a Hypersonic Cruise missileY. Fan, X. Wu, H. Xu, F. Wang, Northwestern Polytechnical University, Xi’an, China

0830 hrsAIAA-2017-2112Four-Loop Feedback Control System with Integrator Design for Hypersonic Cruise MissileH. Xu, Y. Yu, Northwestern Polytechnical University, Xi’an, China; X. Guo, China Aerospace Science and Technology Corporation (CASC), Xi’an, China; F. Wang, Northwestern Polytechnical University, Xi’an, China

0900 hrsAIAA-2017-2113Research on the influence of fluidic thrust vector parameters on the single expansion ramp nozzle of the air-breathing hypersonic vehicleY. Ren, D. Zhang, Northwestern Polytechnical University, Xi’an, China; F. Deng, China Academy of Launch Vehicle Technology, Beijing, China

0930 hrsAIAA-2017-2114Novel Sensor based Backstepping Control for Hypersonic Vehicle with Actuator CompensatorW. Yongchao, S. Zhang, L. Cao, G. Cai, X. Hu, H. Zheng, Xi’an Research Institute of High Technology, Xi’an, China

Tuesday, 7 March 201719-HYTASP-5 Propulsion Components I Concert HallChaired by: V. TALYZIN, TsAGI and Y. ZHAO, National University of Defense Technology0800 hrsAIAA-2017-2115Experimental study on the self-excited oscillation and the forced oscillation of shock train in a rectangular isolatorX. Fan, X. Bing, Y. Wang, T. Yuan, National University of Defense Technology, Changsha, China

0830 hrsAIAA-2017-2116Numerical Simulation and Optimization Design for Kerosene Turbo-Pump with Small Flow RateJ. Xuan, C. Shen, X. Wu, National University of Defense Technology, Changsha, China

0900 hrsAIAA-2017-2117Mode Transition analysis of a Dual-Mode ramjet combustorJ. Li, D. Shen, W. Song, Q. Fu, Northwestern Polytechnical University, Xi’an, China

0930 hrsAIAA-2017-2118Turbine Based Combined Cycle Inlet Mode Transition at Different Operation ConditionsJ. Liu, H. Yuan, N. Ge, Nanjing University of Aeronautics and Astronautics, Nanjing, China

Tuesday, 7 March 201720-HYTASP-6 Propulsion Systems I Multiple Function HallChaired by: U. MEHTA, NASA ARC and F. XING, Xiamen University0800 hrsAIAA-2017-2119Multi-Port Filling of Pulsed Detonation EnginesF. Lu, N. Umapathy, S. Thirumangalath, University of Texas, Arlington, Arlington, TX

0830 hrsAIAA-2017-2120Generation and propagation of auto-ignition flame kernel caused by oblique shock in supersonic flow-fieldX. Wenxiong, H. Yanji, X. Qingyao, Z. Wenli, L. Qian, L. Lan, People’s Liberation Army, Beijing, China

0900 hrsAIAA-2017-2121Numerical Analysis of HyShot Scramjet Model with Different Throat HeightsF. Xing, Y. Zhu, Y. Huang, Xiamen University, Xiamen, China; Y. Yao, University of the West of England, Bristol, United Kingdom

Shen, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia Y. Liu, C. Wen, Hong Kong Polytechnic University, Hong Kong, Hong Kong; H. Liquid DropletInvestigation on Shock Induced Stripping Breakup Process of A AIAA-2017-23690930 hrs

0930 hrsAIAA-2017-2383Experimental Analysis of 14-X B Hypersonic Aerospace Vehicle Compression SystemJ. Martos, Technological Institute of Aeronautics (ITA), São José dos Campos, Brazil; P. Toro, I. Rego, University of São Paulo, São José dos Campos, Brazil

Tuesday, 7 March 201721-HYTASP-7 Test and Evaluation I Conference Room 6Chaired by: N. KUKSHINOV, Central Institute of Aviation Motors (CIAM) and R. LI, Huazhong University of Science and Technology0800 hrsAIAA-2017-2122Multispecies Absorption Measurement in an Ammonium Dinitramide based ThrusterH. Zeng, X. Lin, R. Zheng, L. Chen, China Academy of Aerospace Aerodynamics, Beijing, China; F. Li, X. Yu, Chinese Academy of Sciences, Beijing, China

0830 hrsAIAA-2017-21233D Prototyping Model Design for Experimental Investigation in Hypersonic Shock TunnelT. Marcos, UNIMES, Santos, Brazil; J. Martos, R. Vilela, Technological Institute of Aeronautics, São jose dos campos, Brazil; P. Toro, A. Oliveira, I. Rego, Institute for Advanced Studies, São José dos Campos, Brazil

0900 hrsAIAA-2017-2124Measurement and Calculation of Shock Stand-off Distances over Hypersonic Spheres in CO2D. Liao, S. Liu, H. Jian, A. Xie, Z. Wang, J. Huang, China Aerodynamics Research and Development Center, Mianyang, China

0930 hrsAIAA-2017-2125Numerical investigation of the application of porous material in tandem nozzle supersonic wind tunnelsJ. Wu, R. Li, Huazhong University of Science and Technology, Wuhan, China

Tuesday, 7 March 201722-HYTASP-8 Thermal Management Systems for Vehicles and All Subsystems I Conference Room 2Chaired by: M. KUHN, German Aerospace Center (DLR) and K. ZHANG, Nanjing University of Aeronautics and Astronautics0800 hrsAIAA-2017-2126Experimental Investigation of a Fuel Cooled Combustor: Cooling Efficiency and Coke FormationL. Taddeo, N. Gascoin, K. Chetehouna, National Institute of Applied Sciences (INSA), Bourges, France; A. Ingenito, F. Stella, University of Rome “La Sapienza”, Rome, Italy; M. Bouchez, MBDA, Bourges, France; et al.

0830 hrsAIAA-2017-2127Aerodynamic Heating in Hypersonic Boundary Layer: Role of Dilatational WavesY. Zhu, X. Chen, J. Wu, S. Chen, C. Lee, Peking University, Beijing, China; G. Mohamed, Virginia Commonwealth University, Richmond, VA

0900 hrsAIAA-2017-2128Heat Transfer Experimental Investigation for Piston Rod Sensor in Hydraulic Servo Actuator of Hypersonic Combustion Ramjet Engine Vectoring NozzleZ. Chang, Beihang University, Beijing, China

0930 hrsAIAA-2017-2129Enhanced Heat Sink by Ethanol Assisted Endothermic Catalytic Cracking of Hydrocarbon FuelsX. Guoliang, Y. Cong, S. Chen, C. Wu, X. Wang, T. Zhang, Chinese Academy of Sciences, Dalian, China

Tuesday, 7 March 201723-LEC-2 0800 - 0930 hrs

Program I Topics:

HIFiRE

Progress of a New Large Scale Free-Piston Shock Tunnel

Conference Hall

Moderator: Klaus Hannemann, German Aerospace Center (DLR) Speakers:

Michael SmartUniversity of Queensland

Xing ChenCAAA

Tuesday, 7 March 201724-NW-6 1000 - 1030 hrs

Tuesday Morning Coffee Break Exhibit Hall

Tuesday, 7 March 201725-HYTASP-9 Computational Methods II Conference Room 1Chaired by: V. WARTEMANN, German Aerospace Center and M. SUN, National University of Defense Technology1030 hrsAIAA-2017-2130Separation analysis in a high-speed rotating cylinder for a binary gas mixtureS. Pradhan, Indian Institute of Science, Bengaluru, India

1100 hrsAIAA-2017-2131Effects of Mach number on primary breakup of liquid jets in gas crossflowF. Xiao, M. Sun, N. Liu, H. Zhang, National University of Defense Technology, Changsha, China

1130 hrsAIAA-2017-2132Development of a Local Mathematical Closure Model for Hypersonic Transitional FlowsJ. Xu, J. Bai, L. Qiao, Z. Fu, N. Liu, Northwestern Polytechnical University, Xi’an, China; Y. Zhang, Xi’an Jiaotong University, Xi’an, China; et al.

RBCC and its Related Program of Japan

Makoto YoshidaJAXA

1200 hrsAIAA-2017-2412Modeling of Hypersonic Flow Transition with Consideration of High Temperature Gas EffectsJ. Zhang, L. Wang, S. Fu, Tsinghua University, Beijing, China

Tuesday, 7 March 201726-HYTASP-10 Hypersonic Fundamentals and History II Conference Room 7Chaired by: M. SMART, The University of Queensland and J. REN, Tsinghua University1030 hrsAIAA-2017-2133Boundary Layer Transition Assessment on a Slender High-Speed VehicleJ. Steelant, A. Passaro, V. Fernandez Villace, ESA, Noordwijk, The Netherlands; A. Gubanov, D. Ivanyushkin, Y. Shvalev, TsAGI, Zhukovsky, Russia; et al.

1100 hrsAIAA-2017-2134Effect of pressure gradient on the stability of hypersonic boundary layer flowsJ. Ren, S. Fu, Tsinghua University, Beijing, China

1130 hrsAIAA-2017-2135Hypersonic Skipping Trajectory Planning for High L/D Gliding VehiclesZ. Wang, X. Cheng, H. Li, Beihang University, Beijing, China

1200 hrsAIAA-2017-2136An Efficient Integrated Aerothermoelasticity Analysis System Based on Surrogate-based Reduced Order Modeling for Hypersonic VehiclesX. Chen, G. Zuo, Y. Shi, China Academy of Space Technology, Beijing, China; L. Liu, Beijing Institute of Technology, Beijing, China

Tuesday, 7 March 201727-HYTASP-11 Missions and Vehicles II Conference Room 4Chaired by: A. PROKHOROV, Central Institute of Aviation Motors (CIAM) and G. LI, University of Electronic Science and Technology of China1030 hrsAIAA-2017-2137Comparison of Return Options for Reusable First StagesL. Bussler, M. Sippel, German Aerospace Center (DLR), Bremen, Germany

1100 hrsAIAA-2017-2138Sensitivity Analysis of Performance for Control-Oriented Model of an Air-Breathing Hypersonic VehicleB. Chen, H. Shen, H. Lei, Y. Liu, Y. Lu, Nanjing University of Aeronautics and Astronautics, Nanjing, China

1130 hrsAIAA-2017-2139Practical Guidance Design for the Boost Phase of Hypersonic Vehicle Subject to Terminal Scramjet Transition ConstraintsZ. Yang, K. Zhu, Beijing Aerospace Technology Institute, Beijing, China; M. Sun, Nankai University, Tianjin, China; Z. Wang, University of South Africa, Florida, South Africa

1200 hrsAIAA-2017-2140Research on the design of double swept waveriderC. Liu, P. Bai, Y. Chen, B. Chen, China Academy of Aerospace Aerodynamics, Beijing, China

Tuesday, 7 March 201728-HYTASP-12 Power and Control Systems II Conference Room 5Chaired by: K. KREMEYER, Physics, Materials, and Applied Mathematics Research, LLC and H. YAN, Northwestern Polytechnical University1030 hrsAIAA-2017-2141A Guidance Scheme for Air-launched Solid Launch VehicleZ. Qian, Z. Xu, Northwestern Polytechnical University, Xi’an, China; H. Bei, B. Yan, National Institute of Aerospace, Beijing, China

1100 hrsAIAA-2017-2142Penetration Trajectory Programming for Air-Breathing Hypersonic Vehicles in Cruise Duration with Control Constraints and Flight Dynamics UncertaintiesH. Guo, F. Wenxing, B. Fu, C. Kang, Y. Jie, Northwestern Polytechnical University, Xi’an, China

1130 hrsAIAA-2017-2143Onboard and Analytic Prediction Algorithm of the Range-to-go for the Lifting VehicleY. Yang, L. Liang, H. Wu, Beijing Aerospace Automation Control Institute, Beijing, China; Y. Wang, Huazhong University of Science and Technology, Wuhan, China

1200 hrsAIAA-2017-2144Exploring Hypersonic Flight Vehicle’s Altitude Tracking Control with Attack Angle Constraints Based on Barrier Lyapunov FunctionX. Ma, C. Kang, F. Wenxing, Y. Jie, Northwestern Polytechnical University, Xi’an, China

Tuesday, 7 March 201729-HYTASP-13 Propulsion Components II Concert HallChaired by: V. TALYZIN, TsAGI and Y. ZHAO, National University of Defense Technology1030 hrsAIAA-2017-2145Design and Performances Analysis of the Integrated Curved Cone Waverider-InletX. He, J. Le, China Aerodynamics Research and Development Center, Mianyang, China

1100 hrsAIAA-2017-2146Mixing Characteristics of Fuel Injection in Supersonic Combustor Considering Upstream Streamwise VorticesJ. Teng, X. Zhou, Y. Li, Y. You, Xiamen University, Xiamen, China

1130 hrsAIAA-2017-2147Numerical Study of the Discrete Staggered Staged Sonic Jet Interaction in a Supersonic CrossflowH. Xu, H. Yang, Z. Ye, D. Zhang, Northwestern Polytechnical University, Xi’an, China

1200 hrsAIAA-2017-2148Investigation of the flow field characteristics in a scramjet combustor with the rearwall-expansion cavityZ. Cai, Z. Wang, M. Sun, National University of Defense Technology, Changsha, China; X. Bai, Lund University, Lund, Sweden

Tuesday, 7 March 201730-HYTASP-14 Propulsion Systems II Multiple Function HallChaired by: U. MEHTA, NASA ARC and F. XING, Xiamen University1030 hrsAIAA-2017-2149A Comparative Study on Millimeter-scale Flame Jet and Detonation Diffraction in a Rectangular ChamberJ. He, W. Fan, Y. Chi, J. Zheng, W. Zhang, Northwestern Polytechnical University, Xi’an, China

1100 hrsAIAA-2017-2150Study on the Dynamic Characteristics of the Thrust Measurement System in Pulse Detonation EnginesY. Wang, W. Fan, J. He, Northwestern Polytechnical University, Xi’an, China

1130 hrsAIAA-2017-2151Thermodynamics Cycle analysis of a one-dimensional scramjet model in different combustion modesW. Ma, Z. Yin, C. Pan, B. Li, H. Zhang, Beijing Aerospace Technology Institute, Beijing, China

1200 hrsAIAA-2017-2384Investigation on Combustion Properties in Simplified Wave Rotor Constant Volume CombustorJ. Li, E. Gong, W. Li, Nanjing University of Aeronautics and Astronautics, Nanjing, China; L. Yuan, People’s Liberation Army University of Science and Technology, Nanjing, China

Tuesday, 7 March 201731-HYTASP-15 Test and Evaluation II Conference Room 6Chaired by: N. KUKSHINOV, Central Institute of Aviation Motors (CIAM) and R. LI, Huazhong University of Science and Technology1030 hrsAIAA-2017-2152Experimentally Simulating Gas Giant Entry in an Expansion TubeC. James, D. Gildfind, R. Morgan, S. Lewis, T. Mcintyre, University of Queensland, Brisbane, Australia

1100 hrsAIAA-2017-2153Experiments to determine surface catalytic recombination coefficients of ultra high temperature ceramics in high temperature dissociated flowsL. Liu, Y. Wang, Northwestern Polytechnical University, Xi’an, China; G. Wang, H. Ma, J. Luo, China Aerodynamics Research and Development Center, Mianyang, China

1130 hrsAIAA-2017-2154Multi-parameter measurements approach based on 2-D interferometric Rayleigh scattering with structured illuminationS. Wang, J. Si, Xi’an Jiaotong University, Xi’an, China; Z. Hu, J. Ye, Z. Zhang, J. Shao, Northwest Institute of Nuclear Technology, Xi’an, China; et al.

1200 hrsAIAA-2017-2155Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock TunnelQ. Wang, Chinese Academy of Sciences, Beijing, China; J. Li, North University of China, Taiyuan, China; P. Lu, J. Li, W. Zhao, Z. Jiang, Chinese Academy of Sciences, Beijing, China

Tuesday, 7 March 201732-HYTASP-16 Thermal Management Systems for Vehicles and All Subsystems II Conference Room 2Chaired by: M. KUHN, German Aerospace Center (DLR) and K. ZHANG, Nanjing University of Aeronautics and Astronautics1030 hrsAIAA-2017-2156Heat-augmented Trajectory Optimization of Hypersonic Cruise VehicleW. Wenkai, Z. Hou, D. Liu, J. Yang, L. Chen, B. Zhu, National University of Defense Technology, Changsha, China

1100 hrsAIAA-2017-2157Dimensional Expanding Precise Time Integration (DE-PTI) for Transient Heat Transfer Analysis of Thermal Protection SystemsW. Zhu, J. Liu, J. Yao, N. Hu, Chongqing University, Chongqing, China; J. Xin, China Academy of Launch Vehicle Technology, Beijing, China

Tuesday, 7 March 201733-HYTASP-17 Propulsion Components III Conference HallChaired by: C. MUNDT, Universität der Bunaeswehr München and J. CHANG, Harbin Institute of Technology1030 hrsAIAA-2017-2158Numerical investigation of fuel pre-injection with different injector configurations in hypersonic inletC. Zhu, R. Qiu, R. Chen, Y. You, Xiamen University, Xiamen, China

1100 hrsAIAA-2017-2159Numerical study of curved surface with wall pressure and Mach number distribution using aerodynamic combinationL. Zhang, Q. Chen, Y. Qiu, M. Li, China Academy of Engineering Physics, Mianyang, China; K. Zhang, Nanjing University of Aeronautics and Astronautics, Nanjing, China

1130 hrsAIAA-2017-2160Numerical study on near-blowoff characteristics of cavity-stabilized premixed flames in supersonic flowsH. Wang, P. Li, Y. Zhang, M. Sun, National University of Defense Technology, Changsha, China

1200 hrsAIAA-2017-2161Control Factor of “Separation Bubble” Scale in Hypersonic InletP. Xiong, H. Bai, C. Jun, Z. Wang, China Aerodynamics Research and Development Center, Mianyang, China

Tuesday, 7 March 201734-LUNCH-2 1230 - 1330 hrs

Tuesday Lunch Yifu Restaurant

Tuesday, 7 March 201735-HYTASP-18 Computational Methods III Conference Room 1Chaired by: V. ZAKHAROV, Central Institute of Aviation Motors (CIAM) and W. YAO, Chinese Academy of Sciences, Institute of Mechancis1330 hrsAIAA-2017-2162Numerical Study of Hypersonic Aerodynamics and Heating on a Cylinder at Mach 6L. Chen, Z. Guo, Z. Hou, W. Wenkai, National University of Defense Technology, Changsha, China

1400 hrsAIAA-2017-2163Two Compressibility Corrections to Flamelet/Progress Variable Model for Supersonic CombustionF. Shan, Science and Technology on Space Physics Laboratory, Beijing, China; L. Hou, Tsinghua University, Beijing, China; Z. Chen, J. Chen, B. Su, Science and Technology on Space Physics Laboratory, Beijing, China

1430 hrsAIAA-2017-2164Development of a Navier−Stokes Code for Hypersonic Nonequilibrium SimulationsJ. Hao, Beihang University, Beijing, China; J. Wang, Shandong University, Jinan, China; C. Lee, Beihang University, Beijing, China

1500 hrsAIAA-2017-2165Development of an Efficient Kinetic Particle based Hybrid DSMC - DCL Numerical Approach for Hypersonic Rarefied FlowsM. G, R. Kumar, Indian Institute of Technology Kanpur, Kanpur, India

Tuesday, 7 March 201736-HYTASP-19 Hypersonic Fundamentals and History III Conference Room 7Chaired by: S. HOSDER, Missouri University of Science and Technology and J. WANG, Peking University1330 hrsAIAA-2017-2166Quasi-one-dimensional analysis on thrust performance of ramjet and scramjetS. Huang, Y. Tan, X. Li, H. Ren, H. Li, China Aerodynamics Research and Development Center, Mianyang, China

1400 hrsAIAA-2017-2167Intrusive and Non-Intrusive Quantification of Binary Mixture Composition from Strut Injectors in Supersonic FlowC. Ground, D. Vigano’, L. Maddalena, University of Texas, Arlington, Arlington, TX

1430 hrsAIAA-2017-2168Trajectory-Based Fluid-Thermal-Structural Coupled Analysis for Mars Entry CapsuleX. Yang, L. Liu, G. Dai, W. Tang, Y. Gui, Y. Du, China Aerodynamics Research and Development Center, Mianyang, China

1500 hrsAIAA-2017-2169Analysis of the Maintenance of Elemental Ratio in Hypersonic Thermochemical Nonequilibrium FlowM. Zeng, D. Xu, M. Ge, P. Jin, National University of Defense Technology, Changsha, China

Tuesday, 7 March 201737-HYTASP-20 Missions and Vehicles III Conference Room 4Chaired by: L. SERRE, ONERA and L. CHEN, Chinese Academy of Sciences, Institute of Mechanics1330 hrsAIAA-2017-2170Advanced Simulations of Reusable Hypersonic Rocket-Powered StagesM. Sippel, L. Bussler, A. Kopp, German Aerospace Center (DLR), Bremen, Germany

1400 hrsAIAA-2017-2171Aerodynamic Performance Analysis of A New Conception Hypersonic AircraftX. Ma, S. Zhong, Y. Xiao, W. Li, Z. Zhang, Y. Zhang, China Aerodynamics Research and Development Center, Mianyang, China

1430 hrsAIAA-2017-2172Impulsive Relative Hovering of Space Plane and Trajectory Safety AnalysisC. Bo, J. Yuan, W. Ma, Northwestern Polytechnical University, Xi’an, China; Y. Qian, Beijing University of Technology, Beijing, China

1500 hrsAIAA-2017-2173Aerodynamic configuration design and optimization for hypersonic vehiclesY. Feng, S. Liu, W. Tang, Y. Gui, China Aerodynamics Research and Development Center, Mianyang, China

Tuesday, 7 March 201738-HYTASP-21 Power and Control Systems III Conference Room 5Chaired by: O. GUSKOV, Central Institute of Aviation Motors (CIAM) and T. JACKSON, U.S. Air Force1330 hrsAIAA-2017-2174Strapdown Inertial Navigation Algorithm for Hypersonic Boost-Glide VehicleK. Chen, Northwestern Polytechnical University, Xi’an, China

1400 hrsAIAA-2017-2175A Unified Angle Control Scheme for Hypersonic Vehicle Based on Disturbance RejectionM. Piao, Nankai University, Tianjin, China; K. Zhu, Beijing Aerospace Technology Institute, Beijing, China; M. Sun, Z. Chen, Nankai University, Tianjin, China

1430 hrsAIAA-2017-2176The Research on the Dynamic Decoupling Current Control Algorithm of PMSM in Aerospace Servo SystemZ. Yu, Beijing Research Institute of Precise Mechatronic Controls, Beijing, China; J. Li, National University of Defense Technology, Changsha, China; Y. Du, E. Lu, Beijing Research Institute of Precise Mechatronic Controls, Beijing, China

Tuesday, 7 March 201739-HYTASP-22 Propulsion Systems III Multiple Function HallChaired by: P. LIU, Northwestern Polytechnical University1330 hrsAIAA-2017-2177Design of hypersonic forebody by the combination of bump and waverider surfacesE. Saheby, G. Huang, Nanjing University of Aeronautics and Astronautics, Nanjing, China; A. Hays, California State University, Long Beach, CA

1400 hrsAIAA-2017-2178Analysis of Influence Factors on Performances for Divergent RBCC Engine under the flight condition of Ma3C. Peng, W. Xu, Q. Li, J. Chen, National University of Defense Technology, Changsha, China

1430 hrsAIAA-2017-2179Analysis of the Integral Characteristics of Hexafly-Int Facility ModuleN. Kukshinov, V. Aleksandrov, A. Prokhorov, A. Rudinskiy, Central Institute of Aviation Motors, Moscow, Russia

Tuesday, 7 March 201740-HYTASP-23 Test and Evaluation III Conference Room 6Chaired by: F. CHEN, Shanghai Jiao Tong University and D. WILSON, University of Texas, Arlington1330 hrsAIAA-2017-2180Experimental Study of Hypersonic Flutter of a Blunt-leading-edge Trapezoidal WingC. Ji, W. Jiang, J. Zhu, Z. Liu, F. Li, China Academy of Aerospace Aerodynamics, Beijing, China

1400 hrsAIAA-2017-2181Slot Injection of Hydrogen into a Supersonic Air FlowM. Zhao, D. Buttsworth, R. Choudhury, R. Malpress, University of Southern Queensland, Toowoomba, Australia; F. Xing, Xiamen University, Xiamen, China

1430 hrsAIAA-2017-2333Experimental study on compact heat exchanger for hypersonic aero-engineH. Lee, Y. Chen, Z. Zou, H. Liu, Beihang University, Beijing, China

1500 hrsAIAA-2017-2334Research on Dynamic Derivatives Test Technique for Integrative Hypersonic Vehicle with Internal and External Flow in Wind TunnelJ. Chen, China Aerodynamics Research and Development Center, Mianyang, China

1500 hrsAIAA-2017-2428Detonation interaction with cavity in supersonic combustible mixtureX. Cai, J. Liang, National University of Defense Technology, Changsha, China

Tuesday, 7 March 201741-HYTASP-24 Thermal Management Systems for Vehicles and All Subsystems III Conference Room 2Chaired by: J. LI, Nanjing University of Aeronautics and Astronautics1330 hrsAIAA-2017-2182Evaluation of Heat Flux on HIMICO considering the Ablation of TPST. Miwa, Keio University, Yokohama, Japan; H. Taguchi, Japan Aerospace Exploration Agency (JAXA), Chofu, Japan; A. Matsuo, Keio University, Yokohama, Japan; K. Watanabe, Waseda University, Tokyo, Japan

1400 hrsAIAA-2017-2183Investigation of Probabilistic Design Method for Multi-layer Thermal Protection SystemJ. Xin, China Academy of Launch Vehicle Technology, Beijing, China; J. Yao, Chongqing University, Chongqing, China; W. Hong, Q. Qu, X. Xu, China Academy of Launch Vehicle Technology, Beijing, China

1430 hrsAIAA-2017-2184Thermo-mechanical Analysis and Optimization of Lightweight Corrugated-core Sandwich Integrated Thermal Protection System for Hypersonic VehiclesT. Ji, China Academy of Engineering Physics, Mianyang, China

1500 hrsAIAA-2017-2185Study on the Thermal Characteristics of Composite Phase Change Materials for Thermal ManagementY. Du, G. Xiao, L. Liu, D. Wei, X. Yang, Y. Gui, China Aerodynamics Research and Development Center, Mianyang, China

Tuesday, 7 March 201742-HYTASP-26 Propulsion Components IV Concert HallChaired by: D. MUSIELAK, University of Texas at Arlington and L. YUE, Chinese Academy of Sciences, Institute of Mechanics1330 hrsAIAA-2017-2186Numerical Simulation of Ignition Process in Multi-cavity Combustors at High Supersonic Flight ConditionL. Gao, L. Wang, Z. Qian, Aviation Industry Corporation of China (AVIC), Shenyang, China

1400 hrsAIAA-2017-2187Measurements of the Streamwise Vortices in a Hypersonic Inward Turning InletR. Huang, Z. Li, D. Zhan, J. Yang, University of Science and Technology of China, Hefei, China; A. Yu, W. Yingchuan, China Aerodynamics Research and Development Center, Mianyang, China

1430 hrsAIAA-2017-2188The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting CapabilityY. Jia, L. Yue, X. Zhang, Chinese Academy of Sciences, Beijing, China

1500 hrsAIAA-2017-2189Investigation of ignition, flameholding and combustion characteristics of a kerosene fueled scramjet combustorD. Shi, W. Song, Y. Wang, Q. Fu, Y. Wang, Northwestern Polytechnical University, Xi’an, China

Tuesday, 7 March 201743-NW-7 1530 - 1600 hrs

Tuesday Afternoon Coffee Break Exhibit Hall

Tuesday, 7 March 201744-HYTASP-27 Computational Methods IV Conference Room 1Chaired by: V. ZAKHAROV, Central Institute of Aviation Motors (CIAM) and W. YAO, Chinese Academy of Sciences, Institute of Mechancis1600 hrsAIAA-2017-2190A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy SimulationW. Yao, Y. Yuan, X. Li, J. Wang, X. Fan, Chinese Academy of Sciences, Beijing, China

1630 hrsAIAA-2017-2191The effect of thermal conduction and radiation on the aerodynamic heating of a blunt bodyT. Chen, M. Xu, S. Zeng, E. Quan, L. Liu, Northwestern Polytechnical University, Xi’an, China

1700 hrsAIAA-2017-2192Modeling of Hypersonic Three-Dimensional Boundary Layer Transition Using a Criteria-Based MethodL. Zhou, Huazhong University of Science and Technology, Wuhan, China; R. Zhao, Beijing Institute of Technology, Beijing, China; R. Li, Huazhong University of Science and Technology, Wuhan, China; C. Yan, Beihang University, Beijing, China; W. Zheng, University of Maryland, College Park, College Park, MD

1730 hrsAIAA-2017-2193Topology Structure Stability and Global Stability Analysis of Hypersonic Wake Flow over Blunt bodyZ. Dehua, S. Qing, China Academy of Aerospace Aerodynamics, Beijing, China

Tuesday, 7 March 201745-HYTASP-28 Hypersonic Fundamentals and History IV Conference Room 7Chaired by: S. HOSDER, Missouri University of Science and Technology and C. LI, Northwestern Polytechnical University1600 hrsAIAA-2017-2194Reproducing Non-Uniform Surface Temperature Profiles on Hypersonic Cruise Vehicles in Impulsive Wind TunnelsJ. Vennik, A. Neely, S. Tuttle, University of New South Wales, Canberra, Australia; R. Choudhury, D. Buttsworth, University of Southern Queensland, Toowoomba, Australia

1630 hrsAIAA-2017-2195Thermochemical non-equilibrium effects of shock reflection hysteresis in steady supersonic flowsL. Ji, China Aerodynamics Research and Development Center, Mianyang, China

1700 hrsAIAA-2017-2196Surface Recombination Effects on Aero-heating of High Enthalpy FlowsM. Wenbo, China Academy of Aerospace Aerodynamics, Beijing, China; Y. Yin, China Academy of Launch Vehicle Technology, Beijing, China; C. Nie, Beijing Institute of Near Space Vehicle’s System Engineering, Beijing, China; Y. Dong, X. Cheng, B. Ai, China Academy of Aerospace Aerodynamics, Beijing, China

1730 hrsAIAA-2017-2401Numerical Simulation for the Effects of Angles of Attack on Two- and Three-Dimensional Rarefied Hypersonic Cavity Flows Using the Direct Simulation Monte Carlo MethodX. Jin, F. Huang, X. Cheng, J. Yu, China Academy of Aerospace Aerodynamics, Beijing, China

Tuesday, 7 March 201746-HYTASP-29 Missions and Vehicles IV Conference Room 4Chaired by: L. SERRE, ONERA and L. CHEN, Chinese Academy of Sciences-Institute of Mechanics1600 hrsAIAA-2017-2197Trajectory and guidance scheme design for free flight test of hypersonic vehicleH. Piet-Lahanier, L. Serre, ONERA, Palaiseau, France

1630 hrsAIAA-2017-2198Planform Parameter Study and Wing Twist Distribution Optimization of a Supersonic Transport ConfigurationZ. Fu, J. Bai, N. Liu, Y. Zhang, J. Xu, Northwestern Polytechnical University, Xi’an, China

1700 hrsAIAA-2017-2199Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing WingsL. Guang-li, K. Cui, X. Yao, Y. Xu, Chinese Academy of Sciences, Beijing, China

1730 hrsAIAA-2017-2200Study on Compression Surface Deformation of WaveridersY. Xu, K. Cui, L. Guang-li, X. Yao, Chinese Academy of Sciences, Beijing, China

Tuesday, 7 March 201747-HYTASP-30 Power and Control Systems IV Conference Room 5Chaired by: O. GUSKOV, Central Institute of Aviation Motors (CIAM) and T. JACKSON, U.S. Air Force1600 hrsAIAA-2017-2201A Method of Adaptive Elastic Vibration Suppression for Elastic Slender BodyH. Liu, P. Wang, K. Zhang, Northwestern Polytechnical University, Xi’an, China

1630 hrsAIAA-2017-2202Research on Non-fragile Robust Control of High-Speed Reentry VehicleH. Wu, J. Lian, J. Wu, Beijing Aerospace Automation Control Institute, Beijing, China; Y. Wang, Huazhong University of Science and Technology, Wuhan, China

1700 hrsAIAA-2017-2203Capturability of Retro-Augmented Proportional Navigation Guidance Law Against Higher Speed Maneuvering TargetL. Sun, P. Lian, X. Chang, Northwestern Polytechnical University, Xi’an, China

Tuesday, 7 March 201748-HYTASP-31 Propulsion Systems IV Multiple Function HallChaired by: P. LIU, Northwestern Polytechnical University1600 hrsAIAA-2017-2204RCS and Aerodynamic Parameters Identification of The Reentry Spacecraft from Chang’E Flight TestX. Cheng, R. Xin, L. Wu, Z. Guo, Xiamen University, Xiamen, China

1630 hrsAIAA-2017-2205Studies on the Double-Solution Problem of the Mach Number at the Mixer Outlet of the Supersonic EjectorL. Qi, China Aerodynamics Research and Development Center, Mianyang, China

1700 hrsAIAA-2017-2206IDDES of Supersonic Combustion of Hydrogen and Supercritical Kerosene using Flamelet approachJ. Shin, H. Sung, Korea Aerospace University, Goyang, South Korea

1730 hrsAIAA-2017-2207Study of the Characteristic Mach Number Equivalent Thermo-Process Analysis Method for Dual-mode ScramjetJ. Chen, H. Bai, S. Liu, China Aerodynamics Research and Development Center, Mianyang, China

Tuesday, 7 March 201749-HYTASP-32 Test and Evaluation IV Conference Room 6Chaired by: F. CHEN, Shanghai Jiao Tong University and D. CAO, Harbin Institute of Technology1600 hrsAIAA-2017-2208Main Achievements of the Rocket Technology Flight Experiment ROTEX-TA. Guelhan, German Aerospace Center (DLR), Cologne, Germany

1630 hrsAIAA-2017-2209Unsteady Pressure Measurement of Cavity Flow In a Hypersonic Wind Tunnel Using Fast Response PSPY. JingBo, H. Wang, X. Xiang, China Academy of Aerospace Aerodynamics, Beijing, China

1700 hrsAIAA-2017-2210An Experimental Investigation with Phosphorescent Imaging Technique on Spray Flow in Heated AirF. Chen, Y. Li, H. Meng, Y. Wang, H. Liu, Shanghai Jiao Tong University, Shanghai, China; H. Li, Iowa State University, Ames, IA; et al.

1730 hrsAIAA-2017-2211Development of Ultra-fast Temperature Sensitive Paints for Hypersonic High Speed FlowsJ. Martinez Schramm, F. Edzards, K. Hannemann, German Aerospace Center (DLR), Göttingen, Germany

Tuesday, 7 March 201750-HYTASP-33 Thermal Management Systems for Vehicles and All Subsystems IV Conference Room 2Chaired by: J. LI, Nanjing University of Aeronautics and Astronautics'1600 hrsAIAA-2017-2212Permselectivity Bench to Study Permation Along Porous TubeH. Najmi, National Institute of Applied Sciences (INSA), Bourges, France; E. El Tabach, University of Orléans, Bourges, France; K. Chetehouna, N. Gascoin, L. Lamoot, National Institute of Applied Sciences (INSA), Bourges, France; F. Falempin, MBDA, Paris, France

1630 hrsAIAA-2017-2213Experimental Study on the Layer Properties of RP-3 Oxidation DepositionX. Pei, Nanjing University of Aeronautics and Astronautics, Nanjing, China; L. Hou, Tsinghua University, Beijing, China

1700 hrsAIAA-2017-2214Performance Analysis and Enhancement of Magnetohydrodynamic Heat Shield System For Hypersonic VehiclesK. Li, J. Liu, W. Liu, National University of Defense Technology, Changsha, China

Tuesday, 7 March 201751-HYTASP-34 Propulsion Components V Concert HallChaired by: D. MUSIELAK, University of Texas at Arlington and L. YUE, Chinese Academy of Sciences, Institute of Mechancis1600 hrsAIAA-2017-2215Shock Oscillation and Pressure Fluctuation in Unstarted Hypersonic Inlet FlowL. Xue, C. Wang, Y. Jiao, J. Zhao, K. Cheng, Nanjing University of Aeronautics and Astronautics, Nanjing, China

1630 hrsAIAA-2017-2216Experimental Study of Kerosene Ignition in a Round Scramjet Combustor with Cone-Struts and Cavity Flame HoldersD. Zhang, W. Song, L. Liu, B. Liu, Northwestern Polytechnical University, Xi’an, China

1700 hrsAIAA-2017-2217Design and Research on Parallel-type TBCC 3D NozzleL. Liu, W. Song, D. Zhang, Northwestern Polytechnical University, Xi’an, China

Tuesday, 7 March 201752-PANEL-1 1600 - 1730 hrs

Panel I: Fuel Choice for Hypersonic Civil Transportation Conference Hall

Moderator: Francois Falempin, MBDA Speakers:

Unmeel MehtaNASA

Kevin BowcuttThe Boeing Company

Sergey ChernyshevTsAGI

Guozhu Liu Tianjin University

Laurent SerreONERA

Makoto YoshidaJAXA

WednesdayWednesday, 8 March 201753-SB-2 0730 - 0800 hrs

Wednesday Morning Speaker’s Briefing Session Rooms

Wednesday, 8 March 201754-HYTASP-35 Computational Methods V Conference Room 1Chaired by: M. SMART, The University of Queensland and Z. QIAN, AVIC Aerodynamics Research Institute0800 hrsAIAA-2017-2218Fast Computation Scheme for Gravity Anomaly along Glide Trajectory Based on Extension ApproximationH. Zhou, China Academy of Engineering Physics, Mianyang, China; Z. Ding, China Aerodynamics Research and Development Center, Mianyang, China; W. Zheng, G. Tang, National University of Defense Technology, Changsha, China

0830 hrsAIAA-2017-2219Large eddy simulation of compressibility effects on supersonic boundary layer transition and turbulenceS. Wang, G. Chen, H. Zhen, Z. Zhao, X. Li, Y. Yang, Beijing Institute of Space Long March Vehicle, Beijing, China; et al.

0900 hrsAIAA-2017-2220Numerical Study on Counter-Gradient Transport Phenomenon in Turbulent Premixed FlamesF. Chen, D. Yu, W. Huang, H. Liu, Shanghai Jiao Tong University, Shanghai, China

Wednesday, 8 March 201755-HYTASP-36 Hypersonic Fundamentals and History V Conference Room 7Chaired by: X. YAN, Northwestren Polytechnical University0800 hrsAIAA-2017-2221Experimental investigation on fuel distribution using kerosene-PLIF in a scramjet combustor with dual cavityX. Li, W. Liu, L. Yang, J. Zhu, Y. Pan, National University of Defense Technology, Changsha, China

0830 hrsAIAA-2017-2222Numerical Analysis of the Aerodynamic Heating in Hypersonic Thermo-Chemical Nonequilibrium FlowsJ. Wang, Shandong University, Jinan, China; J. Hao, Beihang University, Beijing, China; G. Du, Shandong University, Jinan, China

0900 hrsAIAA-2017-2223Low Speed Stability Analysis of a Hypersonic Vehicle Design Using CFD and Wind Tunnel TestingJ. Jeyaratnam, T. Bykerk, D. Verstraete, University of Sydney, Sydney, Australia

0930 hrsAIAA-2017-2413Validation of Gas-Kinetic Scheme Solver for the Compressible and Incompressible Flows SimulationH. Liu, Z. Guo, Zhejiang University, Hangzhou, China; K. Xu, Hong Kong University of Science and Technology, Hong Kong, Hong Kong; W. Chen, Zhejiang University, Hangzhou, China

0930 hrsAIAA-2017-2402Experimental Investigation on Flow Characteristic of Combination of Forward-facing Jet and SpikeJ. Zhang, H. Ma, Y. Qin, China Academy of Aerospace Aerodynamics, Beijing, China

Wednesday, 8 March 201756-HYTASP-37 Missions and Vehicles V Conference Room 4Chaired by: A. GUBANOV and Y. XIONG, Beihang University0800 hrsAIAA-2017-2224Vehicle and Mission Design of a Future Small Payload LauncherC. Maddock, F. Toso, L. Ricciardi, A. Mogavero, University of Strathclyde, Glasgow, United Kingdom; K. Lo, S. Rengarajan, University of Glasgow, Glasgow, United Kingdom; et al.

0830 hrsAIAA-2017-2225Dual Waverider Concept for inlet-airframe Integration with Controllable Wall Pressure DistributionY. Li, X. Zheng, J. Teng, Y. You, Xiamen University, Xiamen, China

0900 hrsAIAA-2017-2226Numerical investigation for the effects of gaps and machines on aerodynamic characteristics of a rocketG. Shao Jie, Y. Zhongyan, Z. Peipei, China Academy of Aerospace Aerodynamics, Beijing, China

0930 hrsAIAA-2017-2227Hypersonic aerodynamic characteristics of lifting bodies having variations in body shapeZ. Peipei, Z. Junbo, G. Shao Jie, China Academy of Aerospace Aerodynamics, Beijing, China

Wednesday, 8 March 201757-HYTASP-38 Power and Control Systems V Conference Room 5Chaired by: K. KREMEYER, Physics, Materials, and Applied Mathematics Research, LLC and H. LI, Beihang University0800 hrsAIAA-2017-2228Control Effect of Arc-driven Plasma Synthetic Jet on Supersonic ShockwaveD. Jin, M. Jia, H. Song, Air Force Engineering University, Xi’an, China; Y. Wu, Xi’an Jiaotong University, Xi’an, China; F. Li, Air Force Engineering University, Xi’an, China

0830 hrsAIAA-2017-2229Particle Swarm Optimization for the Hypersonic Vehicle Robust Control System DesignX. Yin, Y. Wang, L. Liu, X. Wei, Huazhong University of Science and Technology, Wuhan, China

0900 hrsAIAA-2017-2230VSC Design For Overload Control In High Angle-of-attack MissileX. Liang, S. Jia, L. Meng, Z. Tong, China Academy of Launch Vehicle Technology, Beijing, China

0930 hrsAIAA-2017-2231Efficient Trajectory Planning for Solid Rocket-Powered Launch Vehicles based on the Newton-Kantorovich/Pseudospectral ApproachX. Cheng, H. Li, R. Zhang, Z. Zhang, Beihang University, Beijing, China

Wednesday, 8 March 201758-HYTASP-39 Propulsion Systems V Multiple Function HallChaired by: N. KUKSHINOV, Central Institute of Aviation Motors (CIAM) and Y. HUANG, Xiamen University0800 hrsAIAA-2017-2232Numerical Simulation of Electric Sail Propulsion in the Ionosphere Plasma EnvironmentG. Xia, Dalian University of Technology, Dalian, China

0830 hrsAIAA-2017-2233Asymmetric Combustion Characteristics of Transverse Ethylene Injection in a Rectangular Supersonic Combustor with Single-side ExpansionM. Sun, Z. Zhong, T. Gao, H. Wang, J. Liang, National University of Defense Technology, Changsha, China

0900 hrsAIAA-2017-2234Detonation Interaction with Boundary Layer in Supersonic Combustible MixtureW. Chen, J. Liang, X. Cai, Z. Lin, National University of Defense Technology, Changsha, China

Wednesday, 8 March 201759-HYTASP-40 Test and Evaluation V Conference Room 6Chaired by: J. MARTINEZ SCHRAMM, DLR - German Aerospace Center and J. LE, China Aerodynamics R&D Center0800 hrsAIAA-2017-2236A New Aerodynamic Layout for Large-scale Conventional Hypersonic Wind TunnelT. Wang, China Academy of Aerospace Aerodynamics, Beijing, China

0830 hrsAIAA-2017-2237Identification of flutter boundary for a hypersonic vehicle wing as X-15 by experiment and numerical simulationL. Guo, J. Lv, C. Ji, D. Chen, China Academy of Aerospace Aerodynamics, Beijing, China

0900 hrsAIAA-2017-2238Some Aspects of Building Effective Automated Process Control Systems Model Hypersonic StandA. Kozerod, M. Kostinskaya, K. Arefyer, M. Ananyan, D. Zhirnov, Moscow Institute of Physics and Technology, Moscow, Russia

Wednesday, 8 March 201760-HYTASP-42 Propulsion Components VI Concert HallChaired by: K. BOWCUTT, The Boeing Company and B. SUN, Nanjing University of Science and Technology0800 hrsAIAA-2017-2239The Application of the Characteristics Tracing MethodH. Liu, Z. Zhou, J. Huang, China Aerodynamics Research and Development Center, Mianyang, China; Y. Zhao, National University of Defense Technology, Changsha, China; J. Yu, China Aerodynamics Research and Development Center, Mianyang, China

0830 hrsAIAA-2017-2240Analytical Modeling of Internal Flow Structures in the Isolator of Scramjet EnginesY. Heo, H. Sung, Korea Aerospace University, Goyang, South Korea

0900 hrsAIAA-2017-2241Experimental Study on Supercritical/Subcritical Injection Characteristics of RP-3 Aviation KeroseneS. Shen, W. Fan, Z. Zhou, L. Jin, J. Zhang, J. Li, Northwestern Polytechnical University, Xi’an, China

0930 hrsAIAA-2017-2242Numerical Investigation on the Performance of the Pulse Detonation Engine with Injected FlowsQ. Zhang, W. Fan, K. Wang, W. Lu, R. Dong, Y. Wang, Northwestern Polytechnical University, Xi’an, China

0930 hrs

Design of a triple combined cycle engineAIAA-2017-2430

Y. Gao, Y. Chen, L. Jia, R. Kang, Northwestern Polytechnical University, Xi’an, China

Wednesday, 8 March 201761-LEC-3 0800 - 0900 hrs

Program II Topics:

Energy-Deposition Program Overview: Enhanced High-Speed Flight Performance

Conference Hall

Moderator: Klaus Hannemann, German Aerospace Center (DLR) Speakers:

Kevin KremeyerPM&AM Research

Wednesday, 8 March 201762-NW-8 1000 - 1030 hrs

Wednesday Morning Coffee Break Exhibit Hall

Wednesday, 8 March 201763-HYTASP-43 Computational Methods VI Conference Room 1Chaired by: M. SMART, The University of Queensland and Z. QIAN, AVIC Aerodynamics Research Institute1030 hrsAIAA-2017-2243A weighted nonlinear filter based high-order finite difference scheme and its application to supersonic jet flowsY. Yang, K. Dinesh, University of Southampton, Southampton, United Kingdom; Z. Wang, M. Sun, H. Wang, National University of Defense Technology, Hunan, China

1100 hrsAIAA-2017-2244Sonic boom signature analysis for a type of hypersonic long-range civil vehicleY. Leng, Z. Qian, Aviation Industry Corporation of China (AVIC), Shenyang, China

1130 hrsAIAA-2017-2245Application of unified gas-kinetic scheme for hypersonic non-equilibrium flowZ. Wang, H. Yan, Northwestern Polytechnical University, Xi’an, China; Q. Li, Tsinghua University, Beijing, China; K. Xu, Hong Kong University of Science and Technology, Hong Kong, Hong Kong

1200 hrsAIAA-2017-2246Numerical dissipation control in an adaptive WCNS scheme for high-speed flowsG. Zhao, M. Sun, National University of Defense Technology, Changsha, China

Wednesday, 8 March 201764-HYTASP-44 Hypersonic Fundamentals and History VI Conference Room 7Chaired by: X. YAN, Northwestren Polytechnical University1030 hrsAIAA-2017-2247Branching and synchronization of fast and slow modes in high-velocity boundary layersZ. Liu, M. Yu, China Academy of Aerospace Aerodynamics, Beijing, China

1100 hrsAIAA-2017-2248Supersonic Film Cooling Simulation with a DG MethodX. Shi, China Academy of Aerospace Aerodynamics, Beijing, China; F. Liu, Beijing Power Machinery Research Institute, Science and Technology on Scramjet Laboratory, Beijing, China; N. Hu, G. Zhang, C. Yue, X. Yuan, China Academy of Aerospace Aerodynamics, Beijing, China

1130 hrsAIAA-2017-2249Experimental Demonstration of Plasma-Based Flameholder in a Model ScramjetS. Leonov, A. Houpt, B. Hedlund, University of Notre Dame, Notre Dame, IN

Wednesday, 8 March 201765-HYTASP-45 Missions and Vehicles VI Conference Room 4Chaired by: A. GUBANOV and Y. XIONG, Beihang University1030 hrsAIAA-2017-2250Return and abort trajectory optimisation for reusable launch vehiclesF. Toso, C. Maddock, University of Strathclyde, Glasgow, United Kingdom

1100 hrsAIAA-2017-2251Trajectory Planning for Cooperative Flight of Two Hypersonic Entry VehiclesZ. Liang, J. Yu, Z. Ren, Q. Li, Beihang University, Beijing, China

1130 hrsAIAA-2017-2252Comparison of Facetted and Blunt Lifting Bodies for Re-Entry FlightV. Wartemann, H. Weihs, T. Eggers, German Aerospace Center (DLR), Braunschweig, Germany

1200 hrsAIAA-2017-2253Separation Modeling Of the Internal Air-Launch Rocket from a Cargo AircraftB. Gao, S. Tang, Z. Xu, Northwestern Polytechnical University, Xi’an, China

The Space Rider: ESA’s Hypersonic Space Transportation System Integrated with VEGA-C

ESAGiorgio Saccoccia

1200 hrsAIAA-2017-2403Study on the influence of aerothermoelasticity deformation on 2-D hypersonic inletD. Guangyue, L. Zeng, H. Jia, L. Liu, B. Qiu, Y. Gui, China Aerodynamics Research and Development Center, Mianyang, China

Wednesday, 8 March 201766-HYTASP-46 Power and Control Systems VI Conference Room 5Chaired by: K. KREMEYER, Physics, Materials, and Applied Mathematics Research, LLC and H. LI, Beihang University1030 hrsAIAA-2017-2254Normal Acceleration Reduce Guidance and Control for Sub-orbit Vehicle Re-entryW. Li, X. Xiao, H. Zhang, Chinese Academy of Sciences, Beijing, China

1100 hrsAIAA-2017-2255On Active Decoupling Control for Horizontal-Lateral Direction of Hypersonic Flight Based on HIFOOS. Ma, Nankai University, Tianjin, China; K. Zhu, Beijing Aerospace Technology Institute, Beijing, China; M. Sun, Nankai University, Tianjin, China; Z. Wang, University of South Africa, Florida, South Africa; Z. Chen, Nankai University, Tianjin, China

1130 hrsAIAA-2017-2256High-altitude and Low-speed Reentry Guidance for Suborbital Reusable Launch Vehicle Returning to Launch SiteH. Lei, X. Yan, Y. Shen, L. Liyang, Northwestern Polytechnical University, Xi’an, China

1200 hrsAIAA-2017-2257A New Strategy to Online Aerodynamic Parameter Identification based on Lyapunov TheoryQ. Huai, X. Xiaobin, China Aerodynamics Research and Development Center, Mianyang, China; L. Tengji, Supersonic Aerodynamic Institute,CARDC, Mianyang, China; S. Peng, G. Leitao, China Aerodynamics Research and Development Center, Mianyang, China

Wednesday, 8 March 201767-HYTASP-47 Propulsion Systems VI Multiple Function HallChaired by: N. KUKSHINOV, Central Institute of Aviation Motors (CIAM) and Y. HUANG, Xiamen University1030 hrsAIAA-2017-2258Transition and turbulence in a wall-bounded channel flow at high Mach numberS. Pradhan, Indian Institute of Science, Bengaluru, India

1100 hrsAIAA-2017-2259Future Prospect of Solar Sails by Comparing Two Light propulsion Sailing SchemesL. Jiang, A. Shi, Z. Qin, Northwestern Polytechnical University, Xi’an, China

1130 hrsAIAA-2017-2260Thermal environment of Pylon at different mode in RBCCD. Yan, G. He, F. Qin, X. Wei, W. Li, Northwestern Polytechnical University, Xi’an, China

1200 hrsAIAA-2017-2261Study on Effects of Fluidic Obstacles on Flame Acceleration and Deflagration-to-Detonation TransitionC. Liu, Y. Huang, W. Yang, H. Peng, F. Xing, Y. You, Xiamen University, Xiamen, China

Wednesday, 8 March 201768-HYTASP-48 Test and Evaluation VI Conference Room 6Chaired by: J. MARTINEZ SCHRAMM, DLR - German Aerospace Center and J. LE, China Aerodynamics R&D Center1030 hrsAIAA-2017-2262Development of hypersonic wind tunnel free-flight test in CAAAZ. Jiang, W. Song, W. Lu, China Academy of Aerospace Aerodynamics, Beijing, China

1100 hrsAIAA-2017-2263Research of Thrust Vector Experimental Simulation Technology and Balance and Air-line Bridge System CalibrationY. Zhang, J. Li, B. Xie, L. Miao, D. Guo, Y. Li, China Aerodynamics Research and Development Center, Mianyang, China

1130 hrsAIAA-2017-2264Aero-propulsion integrated test technique in combustion heated impulse facilityH. Yuanyuan, China Aerodynamics Research and Development Center, Mianyang, China

Wednesday, 8 March 201769-HYTASP-49 Thermal Management Systems for Vehicles and All Subsystems V Conference Room 2Chaired by: D. GLASS, NASA-Langley Research Center and J. LIANG, National University of Defense Technology1030 hrsAIAA-2017-2265Phase-changed transpiration cooling: material selection, permeability analysis, and experimental tests in high heat fluxY. Wu, Beijing Institute of Astronautical Systems Engineering, Beijing, China; G. Zhu, China Academy of Launch Vehicle Technology, Beijing, China; B. Gao, Beijing Institute of Astronautical Systems Engineering, Beijing, China

1100 hrsAIAA-2017-2266Hypersonic Heat Transfer Alleviation Studies on Re Entry VehiclesM. Khalid, K. Juhany, King Abdulaziz University, Jeddah, Saudi Arabia

1130 hrsAIAA-2017-2267Experimental Studies of Film Cooling in Supersonic CombustorsC. Fan, J. Wang, X. Fan, Chinese Academy of Sciences, Beijing, China

1200 hrsAIAA-2017-2268Pressure effect on heat transfer deterioration of accelerating hypersonic vehiclesZ. Liu, J. Liang, Y. Pan, National University of Defense Technology, Changsha, China; L. Cheng, Air Force Engineering University, Xi’an, China

Wednesday, 8 March 201770-HYTASP-50 Propulsion Components VII Concert HallChaired by: M. KUHN, German Aerospace Center (DLR) and B. SUN, Nanjing University of Science and Technology1030 hrsAIAA-2017-2269The design and analysis of Bump in high speed supersonic flowS. Xu, Y. Wang, Z. Wang, X. Fan, National University of Defense Technology, Changsha, China

1100 hrsAIAA-2017-2270Influence of secondary injection parameters on performance of shock vector control nozzleC. He, J. Li, Y. Li, J. Liang, China Aerodynamics Research and Development Center, Mianyang, China

1130 hrsAIAA-2017-2271Numerical Investigation of Pulsed Fuel Injections for the HyShot IIS. Chen, D. Zhao, Nanyang Technological University, Singapore, Singapore

1200 hrsAIAA-2017-2272Aerodynamic Design and Numerical Simulation of An Inward Turning Inlet for Turbine-Based Combined-Cycle EngineH. Min, B. Sun, F. Wu, C. Zhuo, Nanjing University of Science and Technology, Nanjing, China; K. Zhang, Nanjing University of Aeronautics and Astronautics, Nanjing, China

1200 hrsAIAA-2017-2235Enhancement of Free Flight Force Measurement Technique for Scramjet Engine Shock Tunnel TestingK. Hannemann, J. Martinez Schramm, S. Karl, German Aerospace Center (DLR), Göttingen, Germany; S. Laurence, University of Maryland, College Park, College Park, MD

Wednesday, 8 March 201771-HYTASP-51 Propulsion Components VIII Conference HallChaired by: K. BOWCUTT, The Boeing Company and J. QIN, Harbin Institute of Technology1030 hrsAIAA-2017-2273Numerical analysis of scramjet isolator configurations of three different cross-sectional transition functionsF. Cheng, S. Tang, Y. Li, Northwestern Polytechnical University, Xi’an, China

1100 hrsAIAA-2017-2274Detonation attenuation and re-initiation in expanding channelX. Cai, J. Liang, National University of Defense Technology, Changsha, China

1130 hrsAIAA-2017-2275Aerodynamic design and performance analysis of a two-dimensional variable geometry inletH. Yuan, Y. Wang, J. Liu, Z. Hua , Nanjing University of Aeronautics and Astronautics, Nanjing, China

Wednesday, 8 March 201772-LUNCH-3 1230 - 1330 hrs

Wednesday Lunch Yifu Restaurant

Wednesday, 8 March 201773-HYTASP-52 Computational Methods VII Conference Room 1Chaired by: S. HOSDER, Missouri University of Science and Technology and C. ZHU, Xiamen University1330 hrsAIAA-2017-2276Study on Supersonic Base Flow with and without Plume InteractionL. Guoliang, Q. Liu, Y. Yang, A. Gong, Z. Liu, China Academy of Aerospace Aerodynamics, Beijing, China

1400 hrsAIAA-2017-2277Development of zone flamelet model for scramjet combustor modelingW. Yao, X. Fan, Chinese Academy of Sciences, Beijing, China

1430 hrsAIAA-2017-2278Positivity-preserving space-time CE/SE scheme for high speed flowsH. Shen, M. Parsani, King Abdullah University of Science and Technology, Thuwal, Saudi Arabia

1500 hrsAIAA-2017-2279Perfectly Matched Layer Boundary Condition for Nonlinear Euler Equations in General Curvilinear CoordinatesC. Wei, Beijing Aerospace Technology Institute, Beijing, China; S. Wu, Beihang University, Beijing, China; S. Wang, Beijing Aerospace Technology Institute, Beijing, China

Wednesday, 8 March 201774-HYTASP-53 Hypersonic Fundamentals and History VII Conference Room 7Chaired by: A. PROKHOROV, Central Institute of Aviation Motors (CIAM) and Z. LIN, National University of Defense Technology1330 hrsAIAA-2017-2280Numerical Study of Hypersonic Shock-Wave/Laminar Boundary-Layer Interactions of a Typical Lifting VehicleT. Jie, China Academy of Launch Vehicle Technology, Beijing, China

1400 hrsAIAA-2017-2281Measurement technology of model’s positions and attitudes with high accuracy on the 200 m free flight ballistic rangeF. Ke, Z. Wang, China Aerodynamics Research and Development Center, Mianyang, China

1430 hrsAIAA-2017-2282Free Jet Test of Continuous Rotating Detonation Ramjet EngineS. Liu, W. Liu, Y. Wang, Z. Lin, National University of Defense Technology, Changsha, China

Wednesday, 8 March 201775-HYTASP-55 Power and Control Systems VII Conference Room 5Chaired by: N. VOEVODENKO, Central Aerodynamics Institute (TsAGI) and X. YAN, Northwestren Polytechnical University1330 hrsAIAA-2017-2283Blunt Body Shock Wave Control by Radio Frequency Plasma Actuation at Mach 2W. Wang, H. Song, J. Li, D. Jin, M. Jia, Y. Wu, Science and Technology on Plasma Dynamics Laboratory, Xi’an, China

1400 hrsAIAA-2017-2284In-flight Lateral Control Departure Parameter Estimation for Reusable Launch Vehicle Using Retrospective Cost Adaptive ControlQ. Liu, S. Dai, Y. Wang, Y. Wang, C. Min, Science and Technology on Space Physics Laboratory, Beijing, China

1430 hrsAIAA-2017-2285Disturbance Observer Based Back-Stepping Attitude Control for Flexible Hypersonic VehicleL. Yueyong, R. Wang, Harbin Institute of Technology, Harbin, China

Wednesday, 8 March 201776-HYTASP-56 Propulsion Systems VII Multiple Function HallChaired by: W. SONG, Northwestern Polytechnical University1330 hrsAIAA-2017-2286Dynamic Response of a Dual-manifold Injector Rocket Engine for RBCC to Deep ThrottlingP. Cheng, J. Wu, Q. Li, Z. Kang, National University of Defense Technology, Changsha, China

1400 hrsAIAA-2017-2287Experimental Study of Hysteresis Phenomenon for kerosene fueled Supersonic CombustorY. Wang, W. Song, Q. Fu, D. Shi, Y. Wang, Northwestern Polytechnical University, Xi’an, China

1430 hrsAIAA-2017-2288Simulation of kerosene fueled RBCC Engine based on skeletal mechanismB. Liu, G. He, F. Qin, D. Cao, L. Shi, Northwestern Polytechnical University, Xi’an, China

1500 hrsAIAA-2017-2289Performance Analysis of Solid Propellant ATR in Augmented ModeL. Kai, J. Li, Northwestern Polytechnical University, Xi’an, China

1200 hrsAIAA-2017-2422Bladeless turbines for unsteady high speed flows

Purdue University, West Lafayette, IN; B. Le Naour , MBDA, Le Plessis Robinson, F. Falempin, MBDA, Le Plessis Robinson, France; G. Paniagua Perez, J. Braun,

France

1500 hrsAIAA-2017-2404Study on the Aerothermal Characteristics of Supersonic Base FlowX. Sun, China Academy of Launch Vehicle Technology, Beijing, China

Wednesday, 8 March 201777-HYTASP-57 Thermal Management Systems for Vehicles and All Subsystems VI Conference Room 2Chaired by: L. MADDALENA, The University of Texas at Arlington and Y. WU, Xi'an Jiaotong University1330 hrsAIAA-2017-2290Heat Transfer of Kerosene RP-3 Flowing in Vertical Tube at Supercritical PressuresZ. Jia, H. Li, B. Liu, Z. Wu, Beijing Institute of Structure and Environment Engineering, Beijing, China; Y. Fu, Beihang University, Beijing, China

1400 hrsAIAA-2017-2291High Temperature Monitoring by means of Electrical Properties of CMC Materials under Tensile StressT. Staebler, H. Boehrk, H. Voggenreiter, German Aerospace Center (DLR), Stuttgart, Germany

1430 hrsAIAA-2017-2292Design of Flight Path with Minimum Range Based on Circumambulating ManeuverL. Yang, C. Min, L. Ming, Y. Ge, Y. Wang, China Academy of Launch Vehicle Technology, Beijing, China; J. Chen, Harbin Institute of Technology, Harbin, China

1500 hrsAIAA-2017-2293Flight trajectory optimization for TBCC engine thermal management system designD. Lou, H. Yan, J. Zeng, China Gas Turbine Establishment, Chengdu, China

Wednesday, 8 March 201778-HYTASP-58 Propulsion Systems VIII Conference Room 6Chaired by: B. WANG, Tsinghua University1330 hrsAIAA-2017-2294Steady State Characteristics of Scramjet Engines Using Hydrogen for High Mach NumbersZ. Ji, B. Wang, H. Zhang, Tsinghua University, Beijing, China

1400 hrsAIAA-2017-2295Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic CrossflowL. Cheng, F. Zhong, Z. Wang, H. Gu, S. Ma, X. Zhang, Chinese Academy of Sciences, Beijing, China

1430 hrsAIAA-2017-2296Research on Matching Discipline between Primary Rocket and RBCC EngineS. Zheng, China Academy of Launch Vehicle Technology, Beijing, China; X. Lv, Northwestern Polytechnical University, Xi’an, China; Y. Zhang, S. Zhang, China Academy of Launch Vehicle Technology, Beijing, China

Wednesday, 8 March 201779-HYTASP-59 Propulsion Components IX Conference Room 4Chaired by: C. MUNDT, Universität der Bunaeswehr München and J. Wang, Peking University1330 hrsAIAA-2017-2297Compartmental Tank Propellant Management System Design and Operation for Near-space Hypersonic VehicleL. Su, Science and Technology on Space Physics Laboratory, Beijing, China

1400 hrsAIAA-2017-2298Investigation and Control of Unstart Phenomenon in ScramjetsM. Shadab, M. Baig, Aligarh Muslim University, Aligarh, India

1430 hrsAIAA-2017-2299Effect of plasma on the ignition and combustion characteristics of boron containing systemsP. Zhang, Academy of Equipment, Beijing, China; X. Ding, People’s Liberation Army, Beijing, China

1500 hrsAIAA-2017-2300Comparison studies for inverted and no- inverted supersonic inletsD. Cui, S. Zhu, R. Zheng, Beijing Power Machinery Research Institute, Beijing, China

Wednesday, 8 March 201780-HYTASP-60 Propulsion Components X Concert HallChaired by: S. YANG, China Aerodynamics R&D Center1330 hrsAIAA-2017-2301Flow Oscillation in a Scramjet Combustor with Air-ThrottlingS. Yang, Y. Tian, J. Le, China Aerodynamics Research and Development Center, Mianyang, China

1400 hrsAIAA-2017-2302Effects of air-accompanied jets on liquid transvese injected penetration in supersonic crossflowR. Hu, Q. Li, C. Li, C. Li, National University of Defense Technology, Changsha, China

1430 hrsAIAA-2017-2303Investigation on Flow field characteristics of an ethylene fueled scramjet in different combustion modesC. He, J. Xing, B. Xiao, W. Deng, W. Liu, China Aerodynamics Research and Development Center, Mianyang, China


Wednesday Afternoon Coffee Break Exhibit Hall

Wednesday, 8 March 201782-HYTASP-61 Test and Evaluation VII Conference Room 6Chaired by: J. XU, Nanjing University of Aeronautics and Astronautics1600 hrsAIAA-2017-2304Numerical and Experimental Studies of the Support Interference in the Force Prediction of a RBCC Powered VehicleG. Yin, Y. Qin, Y. Yang, China Academy of Launch Vehicle Technology, Beijing, China

1630 hrsAIAA-2017-2305Design and performance of a hypersonic quiet wind tunnel at NUDTD. Gang, S. Yi, X. Lu, National University of Defense Technology, Changsha, China

1700 hrsAIAA-2017-2306Performance of a detonation driven shock tunnelJ. Li, North University of China, Taiyuan, China; W. Qiu, W. Zhao, P. Lu, Chinese Academy of Sciences, Beijing, China; Y. Tan, North University of China, Taiyuan, China

1500 hrsAIAA-2017-2429

J. Qu, F. Luo, Y. Tian, C. Luo, Q. Gang, Beijing Power Machinery Research Institute, Beijing, China

Primary/Secondary Flow Mixing Characteristics in the RBCC Flowpath

Wednesday, 8 March 201783-HYTASP-62 Computational Methods VIII Conference Room 1Chaired by: S. HOSDER, Missouri University of Science and Technology and C. ZHU, Department of aeronautics1600 hrsAIAA-2017-2307Inverse method of characteristics with given exit parameters for the computation of supersonic flowsC. Zhu, R. Qiu, R. Chen, Y. You, Xiamen University, Xiamen, China

1630 hrsAIAA-2017-2308Numerical Study of Influence of High Temperature Effects on Pitch Rotation Derivative for Hypersonic Reentry vehiclesH. Liu, Beihang University, Beijing, China; L. Wei, China Aerospace Science and Industry Corporation (CASIC), Beijing, China; Z. Gao, F. Shi, H. Tang, C. Jiang, Beihang University, Beijing, China; et al.

1700 hrsAIAA-2017-2309Numerical Investigation of Drag Increase due to Roughness Elements in Hypersonic Boundary LayersY. Xue, L. Wang, S. Fu, Tsinghua University, Beijing, China

1730 hrsAIAA-2017-2310Numeric Simulation of Aircraft Gust Response Considering Aeroelastic DeformationJ. Huang, Z. Zhou, H. Liu, China Aerodynamics Research and Development Center, Mianyang, China; Z. Gao, Northwestern Polytechnical University, Xi’an, China; G. Liu, China Aerodynamics Research and Development Center, Mianyang, China

Wednesday, 8 March 201784-HYTASP-63 Hypersonic Fundamentals and History VIII Conference Room 7Chaired by: A. PROKHOROV, Central Institute of Aviation Motors (CIAM) and Z. LIN, National University of Defense Technology1600 hrsAIAA-2017-2311Numerical Investigation of Ultrasonically Absorptive Coating for Hypersonic Laminar Flow ControlP. Lv, China Academy of Aerospace Aerodynamics, Beijing, China; C. Yu, China Academy of Launch Vehicle Technology, Beijing, China; Y. Zhang, J. Gong, China Academy of Aerospace Aerodynamics, Beijing, China

1630 hrsAIAA-2017-2312Study of Graphite TPS for hypersonic flight conditions in high temperature plasma torch flowsK. Arefyer, A. Prokhorov, E. Son, K. Son, Moscow Institute of Physics and Technology, Dolgoprudny, Russia; M. Gadjiev, Joint Institute of High Temperature, Moscow, Russia; J. Kulikov, Moscow Institute of Physics and Technology, Dolgoprudny, Russia

1700 hrsAIAA-2017-2313Periodic Oscillations of Flow Structures in a Supersonic Diffuser PipeX. Li, F. He, Tsinghua University, Beijing, China

1730 hrsAIAA-2017-2314Numerical Study on Distorted Mach Reflection of Strong Moving Shock involving Laminar TransportX. Shi, Y. Zhu, X. Luo, J. Yang, University of Science and Technology of China, Hefei, China

Wednesday, 8 March 201785-HYTASP-64 Missions and Vehicles VII Conference Room 4Chaired by: R. FUSARO, Politecnico di Torino and C. GONG, Northwestern Polytechnincal University1600 hrsAIAA-2017-2315Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted EnginesX. Yao, K. Cui, L. Guang-li, Y. Xu, Chinese Academy of Sciences, Beijing, China

1630 hrsAIAA-2017-2316Numerical and Experimental Aerodynamic Characterization of the HEXAFLY-INT Hypersonic GliderM. Marini, G. Pezzella, A. Schettino, S. Di Benedetto, Italian Aerospace Research Center (CIRA), Capua, Italy; V. Fernandez Villace, J. Steelant, ESA, Noordwijk, The Netherlands; et al.

1700 hrsAIAA-2017-2317Optimization on Interceptor Trajectory for Near Space Hypersonic TargetH. Guo, F. Xie, S. Sun, Science and Technology on Space Physics Laboratory, Beijing, China; C. Huang, Northwestern Polytechnical University, Xi’an, China; Z. Yu, Science and Technology on Space Physics Laboratory, Beijing, China

1730 hrsAIAA-2017-2318The Airframe/Propulsion Integrated Design, Analysis and Ground Test for RBCC Launch VehicleC. Gong, C. Bing, L. Gu, S. Tang, Northwestern Polytechnical University, Xi’an, China

Wednesday, 8 March 201786-HYTASP-65 Power and Control Systems VIII Conference Room 5Chaired by: N. VOEVODENKO, Central Aerodynamics Institute (TsAGI) and X. YAN, Northwestren Polytechnical University1600 hrsAIAA-2017-2319Study on Lateral-Directional Control Strategy for the polarity change of LCDP in flightY. Wang, C. Min, Y. Wang, E. Su, S. Dai, Science and Technology on Space Physics Laboratory, Beijing, China

1630 hrsAIAA-2017-2320Quaternion-Based Reusable Launch Vehicle Composite Attitude Control via Active Disturbance Rejection Control and Sliding Mode ApproachL. Zhang, R. Wu, C. Wei, L. Jing, N. Cui, Harbin Institute of Technology, Harbin, China

1700 hrsAIAA-2017-2321Research on the GFSINS/GPS/CNS integrated navigation technology for hypersonic vehicleY. Ming, L. Ming, Y. Ding, Z. Wei, National University of Defense Technology, Changsha, China; S. Long, Science and Technology on Space Physics Laboratory, Beijing, China

Wednesday, 8 March 201787-HYTASP-66 Propulsion Systems IX Multiple Function HallChaired by: F. LU, University of Texas at Arlington and J. Chang, Harbin Institute of Technology1600 hrsAIAA-2017-2322LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut InjectionK. Wu, P. Zhang, Hong Kong Polytechnic University, Hong Kong, Hong Kong; W. Yao, X. Fan, Chinese Academy of Sciences, Beijing, China

1630 hrsAIAA-2017-2323A direct simulation of continuous detonation engine with the Navier-Stokes equationsL. Zhang, S. Zhang, J. Wang, Peking University, Beijing, China

1700 hrsAIAA-2017-2324Numerical Investigation of Skin-Friction Reduction in a Supersonic ChannelS. Wang, G. He, F. Qin, X. Wei, Z. Huang, Northwestern Polytechnical University, Xi’an, China

1730 hrsAIAA-2017-2325MBDA R&T Effort Regarding Continuous Detonation Wave Engine for Propulsion – Status in 2016B. Le Naour , MBDA, Bourges, France; F. Falempin, MBDA, Le Plessis Robinson, France; K. Coulon, MBDA, Bourges, France

Wednesday, 8 March 201788-HYTASP-68 Propulsion Components XI Concert HallChaired by: S. YANG, China Aerodynamics R&D Center1600 hrsAIAA-2017-2326Experimental and 2.5D numerical investigation of the high-speed combustion chamber within the international HEXAFLY-INT projectV. Talyzin, V. Vlasenko, O. Voloschenko, M. Ivankin, TsAGI, Zhukovsky, Russia

1630 hrsAIAA-2017-2327Effect of outflow vortex of 3D Inlet on fuel injection and mixing in a scramjet combustorX. Zhou, J. Teng, Y. Li, Y. You, Xiamen University, Xiamen, China

1700 hrsAIAA-2017-2328Simulation of the Inlet Pulse-Starting in a Shock Tunnel by

1730 hrsAIAA-2017-2329

Wednesday, 8 March 201789-PANEL-2 1600 - 1730 hrsModerator: Johan Steelant, ESA-ESTEC/NL Speakers:

Unmeel B. MethaNASA

Michael SmartUniversity of Queensland


Thursday, 9 March 201791-SB-3 0730 - 0800 hrs

Thursday, 9 March 201792-HYTASP-69Chaired by: O. GUSKOV, Central Institute of Aviation Motors (CIAM) and B. AI, China Academy of Aerospace Aerodynamics 0800 hrsAIAA-2017-2330Challenge in robust design of composite architectured structures.M. Bouchez, MBDA, Bourges, France; N. Swiergiel, F. Pradat, Airbus, Suresnes, France; A. Larbi, MBDA, Bourges, France

0830 hrsAIAA-2017-2331Thin film deposition using rarefied gas jetS. Pradhan, Indian Institute of Science, Bengaluru, India

Transition of oblique detonation wave in a two-phase hydrocarbon-Decoupling Method air mixtureZ. Li, J. Yang, University of Science and Technology of China, Hefei, China Z. Ren, B. Wang, Tsinghua University, Beijing, China

Panel II: Revolution in Space Launch Vehicles: More Aircraft orLess Rocket? Conference Hall

Martin Sippel Peijin LiuGerman Aerospace Center (DLR) Northwestern Polytechnical University

Gala Dinner Qinye Restaurant, Third Floor

Thursday

Thursday Morning Speakers’ Briefing Session Rooms

Materials and Structures for Vehicles and All Subsystems I Conference Room 2

0900 hrsAIAA-2017-2332Modeling and analysis of functionally graded curved panels in high-speed flow with mutual fluid-thermal-structural couplingW. Kang, Northwestern Polytechnical University, Xi’an, China; K. Li, Xi’an Thermal Power Research Institute, Xi’an, China; X. Dai, Air Force Engineering University, Xi’an, China

Thursday, 9 March 201794-HYTASP-71 Computational Methods IX Conference HallChaired by: F. ZHONG, Chinese Academy of Sciences, Institute of Mechanics 0800 hrsAIAA-2017-2335Numerical Inverstigation on Unsteady Flows with an Air-breathing Hypersonic Vehicle During its Shroud SeparationS. Wang, C. Li, W. Chen, Beijing Aerospace Technology Institute, Beijing, China

0830 hrsAIAA-2017-2336Numerical Studies of 2D Supersonic Reactive Mixing Layer using Hybrid RANS/LES MethodZ. Fan, Z. Zheng, L. Wang, H. Ding, L. Chen, China Aerodynamics Research and Development Center, Mianyang, China

0900 hrsAIAA-2017-2337Hypersonic Natural and Forced Transition Simulation by Correlation-Based IntermittencyM. Yi, H. Zhao, J. Le, China Aerodynamics Research and Development Center, Mianyang, China

0930 hrsAIAA-2017-2414DSMC Simulation of High Mach Number Taylor-Couette FlowS. Pradhan, Indian Institute of Science, Bengaluru, India

Thursday, 9 March 201795-HYTASP-72 Hypersonic Fundamentals and History IX Conference Room 7Chaired by: C. MONJARET, ONERA and Z. YAN, Harbin Institute of Technology0800 hrsAIAA-2017-2338Numerical Investigation of Laminar Separation Induced by Body Flap of Hypersonic VehicleZ. Chen, Z. Ni, J. Wang, China Academy of Aerospace Aerodynamics, Beijing, China

0830 hrsAIAA-2017-2339Numerical Investigation of Unsteady Interaction Characteristic Induced by Impulsive JetJ. Bo, Y. Liu, Y. Liu, China Academy of Aerospace Aerodynamics, Beijing, China

0900 hrsAIAA-2017-2340Energy Deposition to Efficiently Reduce Sonic Boom and Drag, and Increase Control Authority in High-Speed ApplicationsK. Kremeyer, PM&AM Research, Kona, HI; P. Mickelson, E. Montano, PM&AM Research, Tucson, AZ

0930 hrsAIAA-2017-2341Experimental Investigation of Lateral Pulse Jet Interaction Flowfield in Hypersonic FlowZ. Ni, N. Cao, L. Xu, China Academy of Aerospace Aerodynamics, Beijing, China

Thursday, 9 March 201796-HYTASP-73 Missions and Vehicles VIII Conference Room 4Chaired by: A. GUBANOV and R. ZHENG, China Aerospace Science and Industry Corporation 0800 hrsAIAA-2017-2342Exploring Dynamic Characteristics of Steady Turning for Airframe-propulsion Integrated Hypersonic VehicleY. Li, W. Tan, Beihang University, Beijing, China; Y. Wu, Chongqing University, Chongqing, China; X. Qu, L. Sun, Beihang University, Beijing, China

0830 hrsAIAA-2017-2343A Preliminary Research on a Two-Stage-To-Orbit Vehicle with Airbreathing Pre-cooled Hypersonic EnginesJ. Zhou, H. Lu, H. Zhang, L. Zhao, Beijing Aerospace Technology Institute, Beijing, China; J. Chen, R. Zheng, Beijing Power Machinery Research Institute, Beijing, China

0900 hrsAIAA-2017-2344Analysis of longitudinal dynamic characteristics for air-breathing hypersonic flight vehicleY. Li, Beihang University, Beijing, China; Y. Wu, Chongqing University, Chongqing, China; W. Tan, L. Sun, X. Qu, C. Chen, Beihang University, Beijing, China

0930 hrsAIAA-2017-2345Technology Roadmaps Derivation Methodology for European Hypersonic And Re-Entry Space Transportation SystemsS. Cresto Aleina, R. Fusaro, N. Viola, Technical University of Turin, Turin, Italy; J. Longo, G. Saccoccia, ESA, Noordwijk, The Netherlands

Thursday, 9 March 201797-HYTASP-74 Computational Methods X Conference Room 1Chaired by: N. VOEVODENKO, Central Aerodynamics Institute (TsAGI) and Q. LIU, China Academy of Aerospace Aerodynamics0800 hrsAIAA-2017-2346Numerical Simulation of Three-dimensional Non-equilibrium Flows using a Second-order Nonlinear ModelZ. Jiang, W. Chen, W. Zhao, Zhejiang University, Hangzhou, China

0830 hrsAIAA-2017-2347The Computing of Dynamic Derivatives of Hypersonic Lift Body Based on Time Spectral MethodL. Xie, Y. Yang, Z. Liu, W. Zhou, China Academy of Aerospace Aerodynamics, Beijing, China

0900 hrsAIAA-2017-2348An iterative approach to improve Non-intrusive Reduced-Order Models efficiency for parameterized problemsC. Wang, J. Bai, Northwestern Polytechnical University, Xi’an, China; J. Hesthaven, Swiss Federal Institute of Technology, Lausanne, Switzerland

Thursday, 9 March 201798-HYTASP-75 Propulsion Systems X Conference Room 6Chaired by: B. WEI, China Aerospace Science and Industry Corporation and Klaus Hannemann, German Aerospace Center (DLR)0800 hrsAIAA-2017-2349Liquid Rocket Engine Concept for SMILE LauncherI. Müller, M. Kuhn, I. Petkov, German Aerospace Center (DLR), Stuttgart, Germany

0830 hrsAIAA-2017-2350Experimental Investigation on Initiation of Oblique Detonation WavesJ. Gong, Y. Zhang, H. Pan, B. Jia, H. Meng, Academy of Equipment, Beijing, China; X. Lin, Xiamen University, Xiamen, China

0900 hrsAIAA-2017-2351Propulsion Performance Research and status of TRRE Engine experimentB. Wei, W. Ling, F. Luo, Q. Gang, Beijing Power Machinery Research Institute, Beijing, China

0930 hrsAIAA-2017-2352Integrated design and optimization of high speed vehicle and turbine based propulsion systemL. Jia, Y. Chen, Y. Gao, T. Tan, Northwestern Polytechnical University, Xi’an, China

Thursday, 9 March 201799-HYTASP-76 Propulsion Systems XI Conference Room 5Chaired by: F. LU, University of Texas at Arlington and V. TALYZIN, TsAGI0800 hrsAIAA-2017-2353Characterization of Successive Laser Induced Plasma Ignition in an Ethylene Fuelled Model Scramjet EngineL. Yang, B. An, X. Li, National University of Defense Technology, Changsha, China; Y. Yu, X. Li, Harbin Institute of Technology, Harbin, China; J. Liang, National University of Defense Technology, Changsha, China; et al.

0830 hrsAIAA-2017-2354CFD Simulation of TBCC Inlet Based on Internal WaveRider ConceptH. Huihui, G. Huang, Z. Fengyuan, C. Xia, Nanjing University of Aeronautics and Astronautics, Nanjing, China

0900 hrsAIAA-2017-2355Research on Aerodynamically/Mechanically Adjustable ScramjetZ. Huanrong, Y. Chen, Y. Cai, Northwestern Polytechnical University, Xi’an, China

Thursday, 9 March 2017100-HYTASP-77 Propulsion Components XII Concert HallChaired by: B. LE NAOUR , MBDA France and W. FAN, Northwestern Polytechnical University0800 hrsAIAA-2017-2356Numerical Investigation on the Supersonic Hydrogen Jet Flame Affected by ShocksD. Cao, G. He, F. Qin, H. Pan, B. Liu, Z. Huang, Northwestern Polytechnical University, Xi’an, China

0830 hrsAIAA-2017-2357Droplets Evaporation Effects on Scalar Dissipation Rates in Supersonic Turbulent Shear FlowsZ. Ren, B. Wang, Tsinghua University, Beijing, China

0900 hrsAIAA-2017-2358Visualization of Hypersonic Inward-Turning Inlet Flows by Planar Laser Scattering MethodY. Li, Z. Li, J. Yang, University of Science and Technology of China, Hefei, China; W. Yingchuan, A. Yu, China Aerodynamics Research and Development Center, Mianyang, China

Thursday, 9 March 2017101-NW-11 1000 - 1030 hrs

Thursday Morning Coffee Break Exhibit Hall

Thursday, 9 March 2017102-HYTASP-78 Materials and Structures for Vehicles and All Subsystems II Conference Room 2Chaired by: O. GUSKOV, Central Institute of Aviation Motors (CIAM) and B. AI, China Academy of Aerospace Aerodynamics1030 hrsAIAA-2017-2359Model Updating and Uncertainty Propagation in Aerothermoelastic Analysis for C/SiC Panel of Ceramic Matrix CompositeQ. Chen, B. Zhang, J. Yang, G. Su, Xiamen University, Xiamen, China

1100 hrsAIAA-2017-2360Experimental Research of Composite Stiffened Structures in the Structural Design Phase Used in AerospaceL. Mao, Beijing Institute of Structure and Environment Engineering, Beijing, China

1130 hrsAIAA-2017-2361Modeling the heat transfer and mass loss of Si3N4/SiO 2 composite under arc-jet tunnel environmentsJ. Yu, X. Luo, D. Deng, China Academy of Aerospace Aerodynamics, Beijing, China

1200 hrsAIAA-2017-2362Thermal Response of an Ablator: Model and Time Resolved ImagingH. Boehrk, German Aerospace Center (DLR), Stuttgart, Germany

Thursday, 9 March 2017103-HYTASP-79 Test and Evaluation VIII Conference Room 6Chaired by: G. HUANG, Nanjing University of Aeronautics and Astronautics1030 hrsAIAA-2017-2363Numerical Analysis of an Actively-Cooled Low-Reynolds Number Hypersonic DiffuserA. Brune, S. Hosder, Missouri University of Science and Technology, Rolla, MO; D. Campbell, S. Gulli, L. Maddalena, University of Texas, Arlington, Arlington, TX

1100 hrsAIAA-2017-2364An experimental study of thermal buckling behavior in thin-wall structures for hypersonic aircrafts at temperatures up to 1000W. Gong, B. Liu, Z. Jia, H. Cheng, Z. Wu, F. Kong, Beijing Institute of Structure and Environment Engineering, Beijing, China

1130 hrsAIAA-2017-2365Study on the Similarity Criteria of Thermal-Structure Assessment in Wind TunnelL. Liu, Y. Gui, Y. Du, X. Geng, L. He, A. Wang, China Aerodynamics Research and Development Center, Mianyang, China

1200 hrsAIAA-2017-2366Conceptual Study of Compensation of Vitiated Air Heater by Argon EnrichmentD. Cheng, J. Gong, China Academy of Aerospace Aerodynamics, Beijing, China

Xi’an Institute of Aerospace Propulsion Technology, Xi’an , ChinaZhang, Nanjing University of Aeronautics and Astronautics, Nanjing, China; D. Sun, Y. Li, China Aerospace System Development Research Center, Beijing, China; K. Controlled Intake CurveInvestigation of Design Method for the Inward Turning Inlet with AIAA-2017-24230930 hrs

Thursday, 9 March 2017104-HYTASP-80 Hypersonic Fundamentals and History X Conference Room 7Chaired by: C. MONJARET, ONERA and Z. YAN, Harbin Institute of Technology1030 hrsAIAA-2017-2367Static Aerothermoelasticity of Hypersonic VehiclesY. Wang, X. Zhang, China Academy of Aerospace Aerodynamics, Beijing, China

1100 hrsAIAA-2017-2368Research on Interactions Between Cavity and Upstream Transverse Jet in Supersonic CombustorY. Zhao, J. Liang, Y. Zhao, J. Duan, National University of Defense Technology, Changsha, China

1130 hrsAIAA-2017-2370Applications of High-Order Weighted Compact Nonlinear Scheme for Hypersonic Nonequilibrium Flow over Compression CornerM. Ge, M. Zeng, P. Jin, National University of Defense Technology, Changsha, China

Thursday, 9 March 2017105-HYTASP-81 Missions and Vehicles IX Conference Room 4Chaired by: A. GUBANOV and R. ZHENG, China Aerospace Science and Industry Corporation 1030 hrsAIAA-2017-2371Numerical simulation of dynamic deployment of the folding wingY. Ya, China Academy of Launch Vehicle Technology, Beijing, China

1100 hrsAIAA-2017-2372Research on TSTO Reusable Launch Vehicle (RLV) Powered by Turbo-aided RBCC EngineH. Zhang, J. Guo, Y. Xu, B. Du, Y. Wang, W. She, Beijing Aerospace Technology Institute, Beijing, China

1130 hrsAIAA-2017-2373A Review of Uncertainty Analysis for Hypersonic Inflatable Aerodynamic Decelerator DesignA. Brune, Missouri University of Science and Technology, Rolla, MO; T. West, NASA Langley Research Center, Hampton, VA; S. Hosder, Missouri University of Science and Technology, Rolla, MO; K. Edquist, NASA Langley Research Center, Hampton, VA

1200 hrsAIAA-2017-2374Aerodynamic force and heating optimization of HTV-2 typed vehicleJ. Shi, L. Zhang, B. Jiang, B. Ai, China Academy of Aerospace Aerodynamics, Beijing, China

Thursday, 9 March 2017106-HYTASP-82 Computational Methods XI Conference HallChaired by: F. QU, Institute of Manned Space System Engineering1030 hrsAIAA-2017-2375Multidisciplinary design optimization of air propulsion components using principal component analysis methodZ. Lizhang, Z. Yin, Beijing University of Aeronautics and Astronautics, Beijing, China; D. Mi, Y. Zhao, Z. Qian, AECC Hunan Aviation Powerplant Research Institute, Zhuzhou, China

1100 hrsAIAA-2017-2376Fluid-thermal-structural coupling simulation method under hypersonic heating environmentG. Wang, M. Qin, Northwestern Polytechnical University, Xi’an, China; L. Hong, Beijing Institute of Structure and Environment Engineering, Beijing, China

1130 hrsAIAA-2017-2377Developing a Viscoelastic Relaxation Model for AP-HTPB Composite Solid Propellant Based on Experimental DataW. Adel, L. Guozhu, Beihang University, Beijing, China

1200 hrsAIAA-2017-2378Intermittency-based Transition Model with Local Empirical CorrelationsJ. Van den Eynde, J. Steelant, A. Passaro, ESA, Paris, France

Thursday, 9 March 2017107-HYTASP-83 Computational Methods XII Conference Room 1Chaired by: D. WILSON, University of Texas, Arlington and Q. LIU, China Academy of Aerospace Aerodynamics1030 hrsAIAA-2017-2379A Panel Method Aerodynamic Preprocessor for Planetary Entry Trajectory SimulationsN. Donaldson, P. Ireland, University of Oxford, Oxford, United Kingdom

1100 hrsAIAA-2017-2380Numerical Investigation on HIFiRE-5 at Mach 6:Shockwave, Viscosity, and Cross FlowQ. Liu, H. Yu, L. Xie, A. Gong, China Academy of Aerospace Aerodynamics, Beijing, China

1130 hrsAIAA-2017-2381Numerical Investigation of Geometric Parameters Effects on Vortexes and Aerodynamic Heating Environment in Transverse Gaps on Hypersonic VehicleB. Qiu, H. Zhang, Y. Guo, China Aerodynamics Research and Development Center, Mianyang, China

Thursday, 9 March 2017109-HYTASP-85 Propulsion Components XIII Concert HallChaired by: B. LE NAOUR , MBDA France and W. FAN, Northwestern Polytechnical University 1030 hrsAIAA-2017-2385Surface Tuft Flow Visualization in a Hypersonic Inward Turning Inlet/Isolator ModelK. Mu, D. Zhan, Z. Li, R. Huang, J. Yang, University of Science and Technology of China, Hefei, China; W. Yingchuan, China Aerodynamics Research and Development Center, Mianyang, China; et al.

1100 hrsAIAA-2017-2386Influence of Wall Temperature on the Flow Characteristics of a Hypersonic Inward Turning InletE. Zhang, Z. Li, J. Yang, University of Science and Technology of China, Hefei, China; A. Yu, W. Yingchuan, China Aerodynamics Research and Development Center, Mianyang, China

1130 hrsAIAA-2017-2387Experimental Research on Restarting Characteristics of Supersonic Inlet Based of Injection RegulationJ. You, A. Yu, J. Le, S. Yang, X. Rong, F. Li, China Aerodynamics Research and Development Center, Mianyang, China

1200 hrsAIAA-2017-2388Investigations on the Shock Train Structures and UnsteadinessX. Kong, China Aerodynamics Research and Development Center, Mianyang, China

Thursday, 9 March 2017110-HYTASP-86 Propulsion Systems XII Conference Room 5Chaired by: B. WEI, China Aerospace Science and Industry Corporation1030 hrsAIAA-2017-2389Flow Field Manipulation via Fuel Injectors in ScramjetsW. Landsberg, N. Gibbons, V. Wheatley, M. Smart, A. Veeraragavan, University of Queensland, Brisbane, Australia

1100 hrsAIAA-2017-2390Research on Solid Rocket/Scramjet Combined EngineY. He, Y. Chen, Northwestern Polytechnical University, Xi’an, China; D. Liu, J. Liu, M. Lai, X. Liang, Beijing Power Machinery Research Institute, Beijing, China

1130 hrsAIAA-2017-2391Experimental Study on Flame Propagation Characteristics in Multi-Cycle Pulse Detonation Engine with Hot Jet IgnitionW. Zhao, China Aerodynamics Research and Development Center, Mianyang, China; Q. Han, Nanjing University of Aeronautics and Astronautics, Nanjing, China; Q. Li, China Aerodynamics Research and Development Center, Mianyang, China

1200 hrsAIAA-2017-2392Advantage Of Shcramjet Engine At High Mach Number Regime Compared To Scramjet EngineR. Bura, Bandung Institute of Technology, Bandung, Indonesia

Thursday, 9 March 2017111-LUNCH-4 1230 - 1330 hrs

Thursday Lunch Yifu Restaurant

Thursday, 9 March 2017112-HYTASP-87 Materials and Structures for Vehicles and All Subsystems III Conference Room 1Chaired by: D. GLASS, NASA-Langley Research Center and X. QING, Xiamen University1330 hrsAIAA-2017-2393Achievements obtained within ATLLAS-II on Aero-Thermal Loaded Material Investigations for High-Speed VehiclesJ. Steelant, ESA, Noordwijk, The Netherlands; M. Dalenbring, Swedish Defense Research Agency (FOI), Stockholm, Sweden; M. Kuhn, German Aerospace Center (DLR), Stuttgart, Germany; M. Bouchez, MBDA, Bourges, France; J. von Wolfersdorf, University of Stuttgart, Stuttgart, Germany

1400 hrsAIAA-2017-2394High Velocity Impact on Multi-layer MaterialsN. Raju, B. S, R. Gupta, Shiv Nadar University, Greater Noida, India; D. Harusampath, Indian Institute of Science, Bengaluru, India

1430 hrsAIAA-2017-2395Quantification of margins and uncertainties approach for aerothermoelastic analysis based on non-intrusive polynomial chaos methodJ. Yang, B. Zhang, Q. Chen, G. Su, Xiamen University, Xiamen, China

1500 hrsAIAA-2017-2396Study on the application of the hot-wall modified method in fluid-thermal-structure multi fields coupling strategyL. Zeng, G. Dai, Y. Gui, H. Zhang, China Aerodynamics Research and Development Center, Mianyang, China

Thursday, 9 March 2017113-HYTASP-88 Power and Control Systems IX Conference HallChaired by: J. MARTINEZ SCHRAMM, DLR - German Aerospace Center and B. SI, Beijing Institute of Precision Mechatronics and Controls1330 hrsAIAA-2017-2397Investigation of the Shock Wave Generated by DischargeM. Jia, H. Song, D. Jin, Air Force Engineering University, Xi’an, China; Y. Wu, Xi’an Jiaotong University, Xi’an, China; H. Liang, Air Force Engineering University, Xi’an, China

1400 hrsAIAA-2017-2398Research on Multi-model of Hypersonic Vehicle based on Bifurcation TheoryE. Su, C. Min, Z. Xiao, Science and Technology on Space Physics Laboratory, Beijing, China

1430 hrsAIAA-2017-2399Sounding Rocket Roll Control Through DBD Plasma Actuated Boundary Layer ControlS. Sumanik, J. Etele, Carleton University, Ottawa, Canada

1500 hrsAIAA-2017-2400A Reconfigurable drive topology for fault toleranceB. Si, Beijing Research Institute of Precise Mechatronic Controls, Beijing, China; J. Zhu, Tsinghua University, Beijing, China; T. Wang, Hainan University, Haikou, China

Thursday, 9 March 2017115-HYTASP-90 Missions and Vehicles X Conference Room 4Chaired by: N. VIOLA and G. SACCOCCIA1330 hrsAIAA-2017-2405Research on Non-stationary Control of Advanced Hypersonic Morphing VehiclesC. Wei, X. Ju, F. He, Harbin Institute of Technology, Harbin, China; B. Lu, Beijing Institute of Space Long March Vehicle, Beijing, China

1400 hrsAIAA-2017-2406Methodology for the Safety and Reliability assessment of hypersonic transportation systems in conceptual design activitiesR. Fusaro, N. Viola, D. Ferretto, S. Cresto Aleina, M. Fioriti, L. Boggero, Technical University of Turin, Turin, Italy

1430 hrsAIAA-2017-2407Integrated Guidance and Control for Reusable Launch Vehicles with Actuator FailuresH. Lee, C. Wei, N. Cui, Harbin Institute of Technology, Harbin, China; X. Chang, China Aerospace Science and Technology Corporation (CASC), Beijing, China

1500 hrsAIAA-2017-2408The Fast-optimization for Configuration of Hypersonic Vehicle Based on Flight PerformanceL. Ming, Y. Ming, National University of Defense Technology, Changsha, China; Y. Lingxiao, Science and Technology on Space Physics Laboratory, Beijing, China; Y. Ding, National University of Defense Technology, Changsha, China

Thursday, 9 March 2017116-HYTASP-91 Computational Methods XIII Conference Room 7Chaired by: N. VOEVODENKO, Central Aerodynamics Institute (TsAGI) and G. HUANG, Nanjing University of Aeronautics and Astronautics1330 hrsAIAA-2017-2409Numerical Simulations of Hypersonic Boundary Layer Transition Based on the Flow Solver Chant 2.0Y. Zhang, Y. Zhang, J. Chen, M. Mao, Y. Jiang, China Aerodynamics Research and Development Center, Mianyang, China

1400 hrsAIAA-2017-2410Lattice Boltzmann Simulation for Supersonic/Hypersonic Compressible FlowsR. Qiu, Y. You, C. Zhu, R. Chen, Xiamen University, Xiamen, China

1430 hrsAIAA-2017-2411Numerical Modeling and Simulation of Supersonic Flows in Propulsion Systems by Open-Source SolversJ. Hoste , V. Casseau, M. Fossati, University of Strathclyde, Glasgow, United Kingdom; I. Taylor, University of Glasgow, Glasgow, United Kingdom; R. Gollan, University of Queensland, Brisbane, Australia

Thursday, 9 March 2017118-HYTASP-93 Propulsion Components XIV Concert HallChaired by: A. YU, CARDC, P.R.C. and T. EGGERS, DLR Braunschweig1330 hrsAIAA-2017-2415Numerical investigation of two-dimensional supersonic variable-geometry inlet for ramjetY. Pu, G. Huang, Z. Fengyuan, C. Xia, Nanjing University of Aeronautics and Astronautics, Nanjing, China

1400 hrsAIAA-2017-2416Ceramic Strut Injection Technologies for High-Speed FlightM. Kuhn, German Aerospace Center (DLR), Stuttgart, Germany; M. Bouchez, E. Dufour, B. Le Naour , MBDA, Bourges, France; J. Justin, ONERA, Châtillon, France; J. Steelant, ESA, Noordwijk, The Netherlands

1430 hrsAIAA-2017-2417Experimental study on the flow and heat transfer mechanism of the pre-cooler in the hypersonic aeroengineC. Fu, Z. Zou, H. Liu, Beihang University, Beijing, China

1500 hrsAIAA-2017-2418Design and Research of a Wave-rider Inlet Based on a Curved Shock under a Hypersonic Lift-bodyA. Yu, Y. Dawei, T. Wang, China Aerodynamics Research and Development Center, Mianyang, China; H. Yuan, Nanjing University of Aeronautics and Astronautics, Nanjing, China; Y. Wu, J. Le, China Aerodynamics Research and Development Center, Mianyang, China

Thursday, 9 March 2017119-HYTASP-94 Propulsion Systems XIII Conference Room 6Chaired by: R. FUSARO, Politecnico di Torino and J. XU, Nanjing University of Aeronautics and Astronautics1330 hrsAIAA-2017-2419Model for Three-dimensional Distribution of Liquid fuel in Supersonic CrossflowsL. Wu, Y. Chang, K. Zhang, China Aerodynamics Research and Development Center, Mianyang, China; Q. Li, C. Li, National University of Defense Technology, Changsha, China

1400 hrsAIAA-2017-2420An Preliminary Overview analysis on the Internal Waverider Inlets for RamjetZ. Fengyuan, G. Huang, Nanjing University of Aeronautics and Astronautics, Nanjing, China

1430 hrsAIAA-2017-2421Mixing Enhancement Using Secondary Gas Ejection Method in Supersonic-Subsonic Mixing LayerC. Zhang, Y. Liu, X. Yu, Northwestern Polytechnical University, Xi’an, China


Thursday Afternoon Coffee Break Exhibit Hall

Thursday, 9 March 2017122-HYTASP-99 Computational Methods XIV Conference Room 1Chaired by: F. ZHONG Chinese Academy of Sciences (CAS), Institute of Mechancis1600 hrsAIAA-2017-2424Investigation into the influences of the low speeds’ accuracy on RANS simulationsF. Qu, China Academy of Space Technology, Beijing, China; D. Sun, Beihang University, Beijing, China

1630 hrsAIAA-2017-2425A Hybrid Overset Grid Approach Based On Adaptive Cartesian GridS. Liu, China Academy of Aerospace Aerodynamics, Beijing, China

1700 hrsAIAA-2017-2426A Preliminary research on the virtual testing systems of complex vehicleZ. Xiao, Science and Technology on Space Physics Laboratory, Beijing, China; R. Li, Beihang University, Beijing, China; S. Dai, Q. Liu, W. Ying, Science and Technology on Space Physics Laboratory, Beijing, China; N. Li, Beihang University, Beijing, China

1730 hrsAIAA-2017-2427Numerical study of the influence of non-uniform wall temperature distribution on the hypersonic flow over a flat plateJ. de Baar, J. Vennik, A. Neely, University of New South Wales, Canberra, Australia

1500 hrsAIAA-2017-2382Numerical Simulations of Flame Propagation and DDT in Obstructed Detonation Tubes Filled with Fluidic ObstaclesY. Wang, W. Fan, H. Li, Q. Zhang, Northwestern Polytechnical University, Xi’an, China

Thursday, 9 March 2017124-HYTASP-102 Propulsion Components XV Conference Room 7Chaired by: L. SERRE, ONERA and V. TALYZIN, TsAGI1600 hrsAIAA-2017-2431Numerical Investigations on RBCC Variable Inlet in Ma=2-6Z. Zhengze, P. Liu, F. Qin, X. Wei, W. Li, L. Shi, Northwestern Polytechnical University, Xi’an, China

1630 hrsAIAA-2017-2432Investigation on Structure of Shock Wave in the Near-field of a Liquid Jet in M2.1 Supersonic CrossflowC. Li, Q. Li, C. Shen, C. Li, National University of Defense Technology, Changsha, China

1700 hrsAIAA-2017-2433Research on Characteristics of shock train within mixing layer region in Mixer of RBCCG. Yan, Y. Wang, X. Fan, L. Lu, National University of Defense Technology, Changsha, China

1730 hrsAIAA-2017-2434A quasi-one-dimensional analysis method for scramjet combustors with rearwall-expansion cavityY. Zhang, Z. Wang, M. Sun, H. Wang, National University of Defense Technology, Changsha, China

Thursday, 9 March 2017125-HYTASP-103 Propulsion Components XVI Conference Room 6Chaired by: T. EGGERS, DLR Braunschweig and A. YU, China Aerodynamics R&D Center1600 hrsAIAA-2017-2435Effects of the Chemical Nonequilibrium Flow on the Performance of Three Dimensional Expansion NozzleR. Chen, L. Wang, F. Xing, C. Zhu, Y. You, Xiamen University, Xiamen, China

1630 hrsAIAA-2017-2436Downstream pressure variation induced hysteresis in the scramjet isolatorT. Huang, Y. Lianjie, S. Ma, J. Yinan, C. Xinyu, Chinese Academy of Sciences, Beijing, China

1700 hrsAIAA-2017-2437Numerical Simulation of Variable-Geometry Inlet for TRRE Combined Cycle EngineY. Hui, M. Jun, Y. Man, S. Zhu, W. Ling, X. Cao, Academy of Equipment, Beijing, China

1730 hrsAIAA-2017-2438Experimental Investigation of an Over-Under TBCC Exhaust SystemB. Xu, J. Xu, Y. Niu, K. Chen, Nanjing University of Aeronautics and Astronautics, Nanjing, China; X. Wang, W. Zhu, Shenyang Aircraft Design and Research Institute, Shenyang, China

Thursday, 9 March 2017126-HYTASP-97 Missions and Vehicles XI Conference Room 4Chaired by: G. SACCOCCIA and N. VIOLA1600 hrsAIAA-2017-2439Variable Mach Number Design Methodology for the Wide-Speed Range Waverider generated from axisymmetric supersonic flowsS. Li, W. Huang, Z. Wang, T. Zhang, L. Yan, National University of Defense Technology, Changsha, China

1630 hrsAIAA-2017-2440Database on Hypersonic Transportation Systems: a versatile support for the Technology Roadmap generation and Conceptual Design ActivitiesR. Fusaro, S. Cresto Aleina, N. Viola, Technical University of Turin, Turin, Italy; J. Longo, G. Saccoccia, ESA, Noordwijk, The Netherlands

1700 hrsAIAA-2017-2441Innovative European Launcher Concept SMILEM. Kuhn, I. Müller, I. Petkov, German Aerospace Center (DLR), Stuttgart, Germany; B. Oving, A. van Kleef, National Aerospace Laboratory (NLR), Marknesse, The Netherlands; C. Verberne, Nammo Raufoss, Raufoss, Norway; et al.

1730 hrsAIAA-2017-2442Comparison of VTOL and HTHL Hypersonic AircraftsZ. Xiaopeng, C. Haixin, Tsinghua University, Beijing, China

Thursday, 9 March 2017127-HYTASP-100 Computational Methods XV Concert HallChaired by: J. QIN, Harbin Institute of Technology1600 hrsAIAA-2017-2443Mission based Flying Qualities Evaluation of Hypersonic VehiclesY. Luo, Y. Wang, China Academy of Aerospace Aerodynamics, Beijing, China

1630 hrsAIAA-2017-2444A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flowL. Yachao, W. Yao, X. Fan, Chinese Academy of Sciences, Beijing, China

1700 hrsAIAA-2017-2445Investigation into the influences of the low speed’s accuracy on the hypersonic heating predictions for the Reusable Manned Space VehicleF. Qu, China Academy of Space Technology, Beijing, China; D. Sun, Beihang University, Beijing, China; Y. Shi, G. Zuo, China Academy of Space Technology, Beijing, China

1730 hrsAIAA-2017-2446Prediction of Heat Transfer in the Base Region of a High Speed VehicleJ. Yang, China Aerodynamics Research and Development Center, Mianyang, China

Thursday, 9 March 2017128-PANEL-3 1600 - 1730 hrs

Panel III: Conference Impact Conference Hall

Moderator: Yancheng You, Xiamen University Speakers:

Kevin BowcuttThe Boeing Company

David GlassNASA

Richard MorgenUniversity of Queensland

Jian TengXiamen University

Vigor YangGeorgia Institute of Technology

Riheng ZhengChina Aerospace Science & Industry Corporation


Farewell Reception Exhibit Hall

Author/Session Chair IndexAdel, W., 106-HYTASP-82 Ai, B., 45-HYTASP-28, 92-HYTASP-69, 102-HYTASP-78, 105-HYTASP-81 Aleksandrov, V., 39-HYTASP-22 An, B., 99-HYTASP-76 Ananyan, M., 59-HYTASP-40 Arefyev, K., 59-HYTASP-40, 84-HYTASP-63 Bai, H., 33-HYTASP-17, 48-HYTASP-31 Bai, J., 25-HYTASP-9, 46-HYTASP-29, 97-HYTASP-74 Bai, P., 27-HYTASP-11 Bai, X., 29-HYTASP-13 Baig, M., 79-HYTASP-59 Bei, H., 28-HYTASP-12 Benavides, J., 15-HYTASP-1 Bing, C., 16-HYTASP-2, 85-HYTASP-64 Bing, X., 19-HYTASP-5 Bo, C., 37-HYTASP-20 Bo, J., 95-HYTASP-72 Boehrk, H., 77-HYTASP-57, 102-HYTASP-78 Boggero, L., 115-HYTASP-90 Bouchez, M., 22-HYTASP-8, 80-HYTASP-60, 88-HYTASP-68, 92-HYTASP-69, 103-HYTASP-79, 112-HYTASP-87, 118-HYTASP-93 Bowcutt, K., 60-HYTASP-42, 71-HYTASP-51 Braun, J., 71-HYTASP-51 Brune, A., 103-HYTASP-79, 105-HYTASP-81 Bura, R., 110-HYTASP-86 Bussler, L., 27-HYTASP-11, 37-HYTASP-20 Buttsworth, D., 40-HYTASP-23, 45-HYTASP-28 Bykerk, T., 55-HYTASP-36 Cai, G., 18-HYTASP-4 Cai, X., 39-HYTASP-22, 58-HYTASP-39, 71-HYTASP-51

Cai, Y., 99-HYTASP-76 Cai, Z., 29-HYTASP-13 Campbell, D., 103-HYTASP-79 Cao, D., 49-HYTASP-32 Cao, D., 76-HYTASP-56, 100-HYTASP-77 Cao, L., 18-HYTASP-4 Cao, N., 95-HYTASP-72 Cao, X., 125-HYTASP-103 Casseau, V., 116-HYTASP-91 Chang, J., 33-HYTASP-17 Chang, X., 47-HYTASP-30, 115-HYTASP-90 Chang, Y., 119-HYTASP-94 Chang, Z., 22-HYTASP-8 Chen, B., 27-HYTASP-11 Chen, C., 96-HYTASP-73 Chen, D., 59-HYTASP-40 Chen, F., 40-HYTASP-23, 49-HYTASP-32, 54-HYTASP-35

Chen, J., 35-HYTASP-18, 39-HYTASP-22, 40-HYTASP-23, 48-HYTASP-31, 77-HYTASP-57, 96-HYTASP-73, 116-HYTASP-91 Chen, K., 38-HYTASP-21, 125-HYTASP-103 Chen, L., 21-HYTASP-7, 32-HYTASP-16, 35-HYTASP-18, 37-HYTASP-20, 46-HYTASP-29, 94-HYTASP-71 Chen, Q., 33-HYTASP-17, 102-HYTASP-78, 112-HYTASP-87 Chen, R., 33-HYTASP-17, 83-HYTASP-62, 116-HYTASP-91, 125-HYTASP-103 Chen, S., 22-HYTASP-8, 70-HYTASP-50 Chen, T., 44-HYTASP-27 Chen, W., 54-HYTASP-35, 58-HYTASP-39, 94-HYTASP-71, 97-HYTASP-74Chen, X., 22-HYTASP-8, 26-HYTASP-10 Chen, Y., 27-HYTASP-11, 58-HYTASP-39, 93-HYTASP-70, 98-HYTASP-75, 99-HYTASP-76, 110-HYTASP-86,

Chen, Z., 35-HYTASP-18, 38-HYTASP-21, 66-HYTASP-46, 95-HYTASP-72 Cheng, C., 16-HYTASP-2 Cheng, D., 103-HYTASP-79 Cheng, F., 71-HYTASP-51 Cheng, H., 103-HYTASP-79 Cheng, K., 16-HYTASP-2, 51-HYTASP-34 Cheng, L., 69-HYTASP-49, 78-HYTASP-58 Cheng, P., 76-HYTASP-56 Cheng, X., 26-HYTASP-10, 45-HYTASP-28, 48-HYTASP-31, 57-HYTASP-38 Chetehouna, K., 22-HYTASP-8, 50-HYTASP-33 Chi, Y., 30-HYTASP-14 Choudhury, R., 40-HYTASP-23, 45-HYTASP-28 Cong, Y., 22-HYTASP-8 Coulon, K., 87-HYTASP-66 Cresto Aleina, S., 96-HYTASP-73, 115-HYTASP-90, 126-HYTASP-97 Cui, D., 79-HYTASP-59 Cui, H., 15-HYTASP-1 Cui, K., 46-HYTASP-29, 85-HYTASP-64 Cui, N., 15-HYTASP-1, 86-HYTASP-65, 115-HYTASP-90 Dai, G., 36-HYTASP-19, 112-HYTASP-87 Dai, S., 75-HYTASP-55, 86-HYTASP-65, 122-HYTASP-99 Dai, X., 92-HYTASP-69 Dalenbring, M., 112-HYTASP-87 Dawei, Y., 118-HYTASP-93 de Baar, J., 122-HYTASP-99 Dehua, Z., 44-HYTASP-27 Deng, D., 102-HYTASP-78

Deng, W., 80-HYTASP-60 Di Benedetto, S., 85-HYTASP-64 Dinesh, K., 63-HYTASP-43 Ding, H., 94-HYTASP-71 Ding, X., 79-HYTASP-59 Ding, Y., 86-HYTASP-65, 115-HYTASP-90 Ding, Z., 54-HYTASP-35 Donaldson, N., 107-HYTASP-83 Dong, M., 15-HYTASP-1 Dong, R., 60-HYTASP-42 Dong, Y., 45-HYTASP-28 Du, B., 105-HYTASP-81 Du, G., 55-HYTASP-36 Du, Y., 36-HYTASP-19, 38-HYTASP-21, 41-HYTASP-24,

103-HYTASP-79 Duan, J., 104-HYTASP-80 Dufour, E., 118-HYTASP-93 Durant, A., 39-HYTASP-22, 48-HYTASP-31, 94-HYTASP-71, 122-HYTASP-99 Edquist, K., 105-HYTASP-81 Edzards, F., 49-HYTASP-32 Eggers, T., 65-HYTASP-45, 118-HYTASP-93, 125-HYTASP-103 El Tabach, E., 50-HYTASP-33 Etele, J., 113-HYTASP-88 Falempin, F., 50-HYTASP-33, 52-HYTASP-1 71-HYTASP-51, 80-HYTASP-66 Fan, C., 69-HYTASP-49 Fan, W., 30-HYTASP-14, 60-HYTASP-42, 100-HYTASP-77, 109-HYTASP-85, 119-HYTASP-94 Fan, X., 19-HYTASP-5, 44-HYTASP-27, 69-HYTASP-49,

70-HYTASP-50, 73-HYTASP-52, 87-HYTASP-66, 124-HYTASP-102, 127-HYTASP-100 Fan, Y., 18-HYTASP-4 Fan, Z., 94-HYTASP-71 Feng, Y., 37-HYTASP-20 Fengyuan, Z., 99-HYTASP-76, 118-HYTASP-93, 119-HYTASP-94 Fernandez Villace, V., 26-HYTASP-10, 85-HYTASP-64 Ferretto, D., 115-HYTASP-90 Fioriti, M., 115-HYTASP-90 Forbes-Spyratos, S., 17-HYTASP-3 Fossati, M., 116-HYTASP-91 Fu, B., 28-HYTASP-12 Fu, C., 118-HYTASP-93 Fu, Q., 19-HYTASP-5, 42-HYTASP-26, 76-HYTASP-56 Fu, S., 25-HYTASP-9, 26-HYTASP-10, 83-HYTASP-62 Fu, Y., 77-HYTASP-57

Fusaro, R., 85-HYTASP-64, 96-HYTASP-73, 115-HYTASP-90, 119-HYTASP-94, 123-HYTASP-101, 126-HYTASP-97 G, M., 35-HYTASP-18 Gadjiev, M., 84-HYTASP-63 Gang, D., 82-HYTASP-61 Gang, Q., 78-HYTASP-58, 98-HYTASP-75 Gao, B., 65-HYTASP-45, 69-HYTASP-49 Gao, L., 42-HYTASP-26 Gao, T., 58-HYTASP-39 Gao, Y., 58-HYTASP-39, 98-HYTASP-75Gao, Z., 83-HYTASP-62 Gascoin, N., 22-HYTASP-8, 50-HYTASP-33 Ge, M., 36-HYTASP-19, 104-HYTASP-80 Ge, N., 19-HYTASP-5 Ge, Y., 77-HYTASP-57 Geng, X., 103-HYTASP-79 Gibbons, N., 110-HYTASP-86 Gildfind, D., 31-HYTASP-15 Glass, D., 69-HYTASP-49, 112-HYTASP-87 Gollan, R., 116-HYTASP-91 Gong, A., 73-HYTASP-52, 107-HYTASP-83 Gong, C., 16-HYTASP-2, 85-HYTASP-64 Gong, E., 30-HYTASP-14 Gong, J., 84-HYTASP-63, 98-HYTASP-75, 103-HYTASP-79 Gong, W., 103-HYTASP-79 Ground, C., 36-HYTASP-19 Gu, H., 78-HYTASP-58 Gu, L., 16-HYTASP-2, 85-HYTASP-64 Guan, B., 16-HYTASP-2 Guang-li, L., 46-HYTASP-29, 85-HYTASP-64 Guangyue, D., 64-HYTASP-44 Gubanov, A., 26-HYTASP-10, 56-HYTASP-37, 65-HYTASP-45, 96-HYTASP-73, 105-HYTASP-81 Guelhan, A., 49-HYTASP-32 Gui, Y., 36-HYTASP-19, 37-HYTASP-20, 41-HYTASP-24, 64-HYTASP-44, 103-HYTASP-79, 112-HYTASP-87Gulli, S., 103-HYTASP-79 Guo, D., 68-HYTASP-48 Guo, H., 28-HYTASP-12, 85-HYTASP-64 Guo, J., 105-HYTASP-81 Guo, L., 59-HYTASP-40 Guo, X., 18-HYTASP-4 Guo, Y., 107-HYTASP-83 Guo, Z., 35-HYTASP-18, 48-HYTASP-31, 54-HYTASP-35 Guoliang, L., 73-HYTASP-52 Guoliang, X., 22-HYTASP-8

Guskov, O., 38-HYTASP-21, 47-HYTASP-30, 92-HYTASP-69, 102-HYTASP-78 Haixin, C., 126-HYTASP-97 Han, Q., 110-HYTASP-86 Hannemann, K., 23-LEC-2,49-HYTASP-32

Hao, J., 35-HYTASP-18, 55-HYTASP-36 Hao, Q., 17-HYTASP-3 Harusampath, D., 112-HYTASP-87 Hays, A., 39-HYTASP-22 He, C., 70-HYTASP-50, 80-HYTASP-60 He, F., 84-HYTASP-63, 115-HYTASP-90 He, G., 67-HYTASP-47, 76-HYTASP-56, 87-HYTASP-66,

100-HYTASP-77 He, J., 30-HYTASP-14 He, L., 103-HYTASP-79 He, X., 29-HYTASP-13 He, Y., 110-HYTASP-86 Hedlund, B., 64-HYTASP-44 Heo, Y., 60-HYTASP-42 Hesthaven, J., 97-HYTASP-74 Hong, L., 106-HYTASP-82 Hong, W., 41-HYTASP-24 Hosder, S., 36-HYTASP-19, 45-HYTASP-28, 73-HYTASP-52, 83-HYTASP-62, 103-HYTASP-79, 105-HYTASP-81 Hoste, J., 116-HYTASP-91 Hou, L., 35-HYTASP-18, 50-HYTASP-33 Hou, Z., 32-HYTASP-16, 35-HYTASP-18 Houpt, A., 64-HYTASP-44 Hu, N., 32-HYTASP-16, 64-HYTASP-44 Hu, R., 80-HYTASP-60 Hu, X., 18-HYTASP-4 Hu, Z., 31-HYTASP-15 Hua, Z., 71-HYTASP-51 Huai, Q., 66-HYTASP-46 Huang, C., 85-HYTASP-64 Huang, F., 45-HYTASP-28 Huang, G., 39-HYTASP-22, 99-HYTASP-76,103-HYTASP-79, 116-HYTASP-91, 118-HYTASP-93, 119-HYTASP-94,

123-HYTASP-101 Huang, J., 21-HYTASP-7, 60-HYTASP-42, 83-HYTASP-62 Huang, R., 42-HYTASP-26, 109-HYTASP-85 Huang, S., 36-HYTASP-19 Huang, T., 125-HYTASP-103 Huang, W., 54-HYTASP-35, 126-HYTASP-97 Huang, Y., 20-HYTASP-6, 58-HYTASP-39, 67-HYTASP-47

61-LEC-3 , 68-HYTASP-48, 98-HYTASP-75

Gupta, R., 112-HYTASP-87 Guozhu, L., 106-HYTASP-82 Fu, Z., 25-HYTASP-9, 46-HYTASP-29 Deng, F., 18-HYTASP-4 Chen, G., 54-HYTASP-35

Author/Session Chair Index

Huihui, H., 99-HYTASP-76 Huo, L., 16-HYTASP-2 Ingenito, A., 22-HYTASP-8 Ireland, P., 107-HYTASP-83 Ivankin, M., 88-HYTASP-68 Ivanyushkin, D., 26-HYTASP-10 Jackson, T., 38-HYTASP-21, 47-HYTASP-30 Jahn, I., 17-HYTASP-3 James, C., 31-HYTASP-15 Jeyaratnam, J., 55-HYTASP-36 Ji, C., 40-HYTASP-23, 59-HYTASP-40 Ji, L., 45-HYTASP-28 Ji, T., 41-HYTASP-24 Ji, Z., 78-HYTASP-58 Jia, B., 98-HYTASP-75 Jia, H., 64-HYTASP-44 Jia, L., 58-HYTASP-39, 98-HYTASP-75Jia, M., 57-HYTASP-38, 75-HYTASP-55, 113-HYTASP-88 Jia, S., 57-HYTASP-38 Jia, Y., 42-HYTASP-26 Jia, Z., 77-HYTASP-57, 103-HYTASP-79 Jian, H., 21-HYTASP-7 Jiang, B., 105-HYTASP-81 Jiang, C., 83-HYTASP-62 Jiang, L., 67-HYTASP-47 Jiang, W., 40-HYTASP-23 Jiang, Y., 116-HYTASP-91 Jiang, Z., 31-HYTASP-15, 68-HYTASP-48, 97-HYTASP-74 Jianping, W., 71-HYTASP-51, 79-HYTASP-59 Jiao, S., 15-HYTASP-1 Jiao, Y., 16-HYTASP-2, 51-HYTASP-34 Jie, T., 74-HYTASP-53 Jie, Y., 28-HYTASP-12 Jin, D., 57-HYTASP-38, 75-HYTASP-55, 113-HYTASP-88 Jin, L., 60-HYTASP-42 Jin, P., 36-HYTASP-19, 104-HYTASP-80 Jin, X., 45-HYTASP-28 Jing, L., 86-HYTASP-65 JingBo, Y., 49-HYTASP-32 Ju, X., 115-HYTASP-90 Juhany, K., 69-HYTASP-49 Jun, C., 33-HYTASP-17 Jun, M., 125-HYTASP-103 Junbo, Z., 56-HYTASP-37 Justin, J., 118-HYTASP-93 Kai, L., 76-HYTASP-56

Kang, Z., 76-HYTASP-56

Ke, F., 74-HYTASP-53 Kearney, M., 17-HYTASP-3 Khalid, M., 69-HYTASP-49 Kong, F., 103-HYTASP-79 Kong, X., 109-HYTASP-85 Kopp, A., 37-HYTASP-20 Kostinskaya, M., 59-HYTASP-40 Kozerod, A., 59-HYTASP-40 Kremeyer, K., 18-HYTASP-4, 28-HYTASP-12, 57-HYTASP-38, 66-HYTASP-46, 95-HYTASP-72 Kuhn, M., 22-HYTASP-8, 32-HYTASP-16, 70-HYTASP-50, 98-HYTASP-75, 112-HYTASP-87, 118-HYTASP-93, 126-HYTASP-97 Kukshinov, N., 21-HYTASP-7, 31-HYTASP-15, 39-HYTASP-22, 58-HYTASP-39, 67-HYTASP-47 Kulikov, J., 84-HYTASP-63 Kumar, R., 35-HYTASP-18 Lai, M., 110-HYTASP-86 Lamoot, L., 50-HYTASP-33 Lan, L., 20-HYTASP-6 Landsberg, W., 110-HYTASP-86 Larbi, A., 92-HYTASP-69 Laurence, S., 68-HYTASP-48 Le, J., 15-HYTASP-1, 29-HYTASP-13, 59-HYTASP-40, 68-HYTASP-48, 80-HYTASP-60, 94-HYTASP-71, 109-HYTASP-85, 118-HYTASP-93 Lee, C., 22-HYTASP-8, 35-HYTASP-18 Lee, H., 93-HYTASP-70, 115-HYTASP-90 Lei, H., 27-HYTASP-11, 66-HYTASP-46 Leitao, G., 66-HYTASP-46 Le Naour, B., 71-HYTASP-51, 87-HYTASP-66,

100-HYTASP-77,

109-HYTASP-85, 118-HYTASP-93 Leng, Y., 63-HYTASP-43 Leonov, S., 64-HYTASP-44 Lewis, S., 31-HYTASP-15 Leyva, I., 41-HYTASP-24, 50-HYTASP-33, 76-HYTASP-56 Li, B., 30-HYTASP-14 Li, C., 36-HYTASP-19, 45-HYTASP-28, 80-HYTASP-60, 94-HYTASP-71, 119-HYTASP-94, 124-HYTASP-102 Li, F., 21-HYTASP-7, 40-HYTASP-23, 57-HYTASP-38, 109-HYTASP-85 Li, G., 17-HYTASP-3, 27-HYTASP-11 Li, H., 26-HYTASP-10, 36-HYTASP-19, 49-HYTASP-32, 57-HYTASP-38, 66-HYTASP-46, 77-HYTASP-57,

Karl, S., 68-HYTASP-48

119-HYTASP-94

Li, J., 19-HYTASP-5, 30-HYTASP-14, 31-HYTASP-15, 38-HYTASP-21,

41-HYTASP-24, 50-HYTASP-33,

75-HYTASP-55, 76-HYTASP-56, 82-HYTASP-61, 93-HYTASP-70

Li, K., 50-HYTASP-33, 92-HYTASP-69 Li, M., 33-HYTASP-17 Li, N., 122-HYTASP-99 Li, P., 33-HYTASP-17 Li, Q., 39-HYTASP-22, 63-HYTASP-43, 65-HYTASP-45, 76-HYTASP-56, 80-HYTASP-60, 110-HYTASP-86, 119-HYTASP-94, 124-HYTASP-102 Li, R., 21-HYTASP-7, 31-HYTASP-15, 44-HYTASP-27, 122-HYTASP-99 Li, S., 15-HYTASP-1, 126-HYTASP-97 Li, W., 30-hytasp-14, 37-HYTASP-20, 66-HYTASP-46,

67-HYTASP-47,

124-HYTASP-102 Li, X., 36-HYTASP-19, 44-HYTASP-27, 54-HYTASP-35, 55-HYTASP-36, 84-HYTASP-63, 99-HYTASP-76 Li, Y., 29-HYTASP-13, 49-HYTASP-32, 56-HYTASP-37, 68-HYTASP-48, 70-HYTASP-50, 71-HYTASP-51, 88-HYTASP-68, 96-HYTASP-73, 100-HYTASP-77, 100-HYTASP-77 Li, Z., 42-HYTASP-26, 88-HYTASP-68, 100-HYTASP-77, 109-HYTASP-85 Lian, J., 47-HYTASP-30 Lian, P., 47-HYTASP-30 Liang, H., 113-HYTASP-88 Liang, J., 39-HYTASP-22, 58-HYTASP-39, 69-HYTASP-49, 70-HYTASP-50, 71-HYTASP-51, 99-HYTASP-76, 104-HYTASP-80Liang, L., 28-HYTASP-12 Liang, X., 57-HYTASP-38, 110-HYTASP-86 Liang, Z., 65-HYTASP-45 Lianjie, Y., 125-HYTASP-103 Liao, D., 21-HYTASP-7 Lin, X., 21-HYTASP-7, 98-HYTASP-75 Lin, Z., 58-HYTASP-39, 74-HYTASP-53, 84-HYTASP-63 Ling, W., 98-HYTASP-75, 125-HYTASP-103 Lingxiao, Y., 115-HYTASP-90 Liu, B., 51-HYTASP-34, 76-HYTASP-56, 77-HYTASP-57, 100-HYTASP-77, 103-HYTASP-79 Liu, C., 27-HYTASP-11, 67-HYTASP-47 Liu, D., 32-HYTASP-16, 110-HYTASP-86 Liu, F., 64-HYTASP-44 Liu, G., 83-HYTASP-62 Liu, H., 47-HYTASP-30, 49-HYTASP-32, 54-HYTASP-35, 60-HYTASP-42, 83-HYTASP-62, 93-HYTASP-70, 118-HYTASP-93 Liu, J., 19-HYTASP-5, 32-HYTASP-16, 50-HYTASP-33, 71-HYTASP-51, 110-HYTASP-86

Liu, L., 26-HYTASP-10, 31-HYTASP-15, 36-HYTASP-19, 41-HYTASP-24, 44-HYTASP-27, 51-HYTASP-34, 57-HYTASP-38, 64-HYTASP-44, 103-HYTASP-79 Liu, N., 25-HYTASP-9, 46-HYTASP-29 Liu, P., 39-HYTASP-22, 48-HYTASP-31, 124-HYTASP-102 Liu, Q., 73-HYTASP-52, 75-HYTASP-55, 97-HYTASP-74, 107-HYTASP-83, 122-HYTASP-99 Liu, S., 21-HYTASP-7, 37-HYTASP-20, 48-HYTASP-31, 74-HYTASP-53, 122-HYTASP-99 Liu, W., 50-HYTASP-33, 55-HYTASP-36, 74-HYTASP-53, 80-HYTASP-60 Liu, Y., 16-HYTASP-2, 27-HYTASP-11, 95-HYTASP-72, 119-HYTASP-94 Liu, Z., 40-HYTASP-23, 64-HYTASP-44, 69-HYTASP-49, 73-HYTASP-52, 97-HYTASP-74 Liyang, L., 66-HYTASP-46 Lizhang, Z., 106-HYTASP-82 Lo, K., 56-HYTASP-37 Long, S., 86-HYTASP-65 Longo, J., 96-HYTASP-73, 126-HYTASP-97 Lou, D., 77-HYTASP-57 Lu, B., 115-HYTASP-90 Lu, E., 38-HYTASP-21 Lu, F., 20-HYTASP-6, 87-HYTASP-66, 99-HYTASP-76 Lu, H., 96-HYTASP-73 Lu, L., 124-HYTASP-102 Lu, P., 31-HYTASP-15, 82-HYTASP-61 Lu, W., 60-HYTASP-42, 68-HYTASP-48 Lu, X., 82-HYTASP-61 Lu, Y., 27-HYTASP-11 Luo, C., 78-HYTASP-58 Luo, F., 78-HYTASP-58, 98-HYTASP-75 Luo, J., 31-HYTASP-15 Luo, X., 84-HYTASP-63, 102-HYTASP-78 Luo, Y., 127-HYTASP-100 Lv, J., 59-HYTASP-40 Lv, P., 84-HYTASP-63 Lv, X., 78-HYTASP-58 Ma, H., 31-HYTASP-15, 55-HYTASP-36Ma, S., 66-HYTASP-46, 78-HYTASP-58, 125-HYTASP-103 Ma, W., 30-HYTASP-14, 37-HYTASP-20 Ma, X., 28-HYTASP-12, 37-HYTASP-20 Maddalena, L., 36-HYTASP-19, 77-HYTASP-57, 103-HYTASP-79, 114-HYTASP-89 Maddock, C., 56-HYTASP-37, 65-HYTASP-45 Malpress, R., 40-HYTASP-23 Man, Y., 125-HYTASP-103 Mao, L., 102-HYTASP-78 Mao, M., 116-HYTASP-91

Marcos, T., 21-HYTASP-7 Marini, M., 85-HYTASP-64 Martinez Schramm, J., 49-HYTASP-32 59-HYTASP-40, 68-HYTASP-48, 113-HYTASP-88 Martos, J., 20-HYTASP-6, 21-HYTASP-7 Matsuo, A., 41-HYTASP-24 Mcintyre, T., 31-HYTASP-15 Mehta, U., 20-HYTASP-6, 30-HYTASP-14, 93-HYTASP-70 Meng, H., 49-HYTASP-32, 98-HYTASP-75 Meng, L., 57-HYTASP-38 Mi, D., 106-HYTASP-82 Miao, L., 68-HYTASP-48 Mickelson, P., 95-HYTASP-72 Min, C., 75-HYTASP-55, 77-HYTASP-57, 86-HYTASP-65, 113-HYTASP-88 Min, H., 70-HYTASP-50 Ming, L., 77-HYTASP-57, 86-HYTASP-65, 115-HYTASP-90 Ming, Y., 86-HYTASP-65, 115-HYTASP-90 Miwa, T., 41-HYTASP-24 Mogavero, A., 56-HYTASP-37 Mohamed, G., 22-HYTASP-8 Monjaret, C., 95-HYTASP-72, 104-HYTASP-80 Montano, E., 95-HYTASP-72 Morgan, R., 31-HYTASP-15 Mu, K., 109-HYTASP-85 Müller, I., 98-HYTASP-75, 126-HYTASP-97 Mundt, C., 33-HYTASP-17, 79-HYTASP-59 Musielak, D., 42-HYTASP-26, 51-HYTASP-34 Najmi, H., 50-HYTASP-33 Neely, A., 45-HYTASP-28, 122-HYTASP-99 Ni, Z., 95-HYTASP-72 Nie, C., 45-HYTASP-28 Niu, Y., 125-HYTASP-103 Oliveira, A., 21-HYTASP-7 Oving, B., 126-HYTASP-97 Pan, C., 30-HYTASP-14 Pan, H., 98-HYTASP-75, 100-HYTASP-77 Pan, Y., 55-HYTASP-36, 69-HYTASP-49 Paniagua Perez, G., 71-HYTASP-51 Parsani, M., 73-HYTASP-52 Passaro, A., 26-HYTASP-10, 106-HYTASP-82 Pei, X., 50-HYTASP-33 Peipei, Z., 56-HYTASP-37 Peng, C., 39-HYTASP-22 Peng, H., 67-HYTASP-47 Peng, S., 17-HYTASP-3, 66-HYTASP-46 Petkov, I., 98-HYTASP-75, 126-HYTASP-97 Pezzella, G., 85-HYTASP-64

60-HYTASP-42, 68-HYTASP-48, 70-HYTASP-50,

Kang, C., 28-HYTASP-12

Kang, W., 92-HYTASP-69 Kang, R., 58-HYTASP-39

Huang, Z., 87-HYTASP-66, 100-HYTASP-77

Hui, Y., 125-HYTASP-103 Huanrong, Z., 99-HYTASP-76

Author/Session Chair IndexPiao, M., 38-HYTASP-21 Piet-Lahanier, H., 46-HYTASP-29 Pradat, F., 92-HYTASP-69 Pradhan, S., 25-HYTASP-9, 67-HYTASP-47, 92-HYTASP-69, 94-HYTASP-71 Prokhorov, A., 17-HYTASP-3, 27-HYTASP-11, 39-HYTASP-22, 74-HYTASP-53, 84-HYTASP-63 Pu, H., 15-HYTASP-1 Pu, Y., 118-HYTASP-93 Qi, L., 48-HYTASP-31 Qian, L., 20-HYTASP-6 Qian, Y., 37-HYTASP-20 Qian, Z., 17-HYTASP-3, 28-HYTASP-12, 42-HYTASP-26, 54-HYTASP-35, 63-HYTASP-43, 106-HYTASP-82 Qiao, L., 25-HYTASP-9 Qin, F., 67-HYTASP-47, 76-HYTASP-56, 87-HYTASP-66, 100-HYTASP-77, 124-HYTASP-102 Qin, J., 71-HYTASP-51, 117-HYTASP-92,

Qin, K., 17-HYTASP-3 Qin, M., 106-HYTASP-82 Qin, Y., 55-HYTASP-36, 82-HYTASP-61 Qin, Z., 67-HYTASP-47 Qing, S., 44-HYTASP-27 Qing, X., 112-HYTASP-87 Qingyao, X., 20-HYTASP-6 Qiu, B., 64-HYTASP-44, 107-HYTASP-83 Qiu, R., 33-HYTASP-17, 83-HYTASP-62, 116-HYTASP-91 Qiu, W., 82-HYTASP-61 Qiu, Y., 33-HYTASP-17 Qu, F., 106-HYTASP-82, 117-HYTASP-92, 122-HYTASP-99, 127-HYTASP-100 Qu, J., 78-HYTASP-58 Qu, Q., 41-HYTASP-24 Qu, X., 96-HYTASP-73 Quan, E., 44-HYTASP-27 Raju, N., 112-HYTASP-87 Rego, I., 20-HYTASP-6, 21-HYTASP-7 Ren, H., 36-HYTASP-19 Ren, J., 16-HYTASP-2, 26-HYTASP-10 Ren, Y., 18-HYTASP-4 Ren, Z., 65-HYTASP-45, 88-HYTASP-68, 100-HYTASP-77 Rengarajan, S., 56-HYTASP-37 Ricciardi, L., 56-HYTASP-37 Rong, X., 109-HYTASP-85 Rudinskiy, A., 39-HYTASP-22 S, B., 112-HYTASP-87 Saccoccia, G., 96-HYTASP-73, 115-HYTASP-90, 126-HYTASP-97

Saheby, E., 39-HYTASP-22 Schettino, A., 85-HYTASP-64 Serre, L., 37-HYTASP-20, 46-HYTASP-29, 120-HYTASP-95, 124-HYTASP-102 Shadab, M., 79-HYTASP-59 Shan, F., 35-HYTASP-18 Shang, Y., 15-HYTASP-1 Shao, J., 31-HYTASP-15 Shao Jie, G., 56-HYTASP-37 She, W., 105-HYTASP-81 Shen, C., 19-HYTASP-5, 124-HYTASP-102 Shen, D., 19-HYTASP-5 Shen, H., 16-HYTASP-2, 27-HYTASP-11, 73-HYTASP-52

Shen, S., 60-HYTASP-42 Shen, Y., 66-HYTASP-46 Shi, A., 67-HYTASP-47 Shi, D., 42-HYTASP-26, 76-HYTASP-56 Shi, F., 83-HYTASP-62 Shi, J., 105-HYTASP-81 Shi, L., 76-HYTASP-56, 124-HYTASP-102 Shi, X., 64-HYTASP-44, 84-HYTASP-63 Shi, Y., 26-HYTASP-10, 127-HYTASP-100 Shin, J., 48-HYTASP-31 Shvalev, Y., 26-HYTASP-10 Si, B., 113-HYTASP-88 Si, J., 31-HYTASP-15

Sippel, M., 27-HYTASP-11, 37-HYTASP-20 Smart, M., 16-HYTASP-2, 17-HYTASP-3, 26-HYTASP-10, 54-HYTASP-35, 63-HYTASP-43, 110-HYTASP-86 Son, E., 84-HYTASP-63 Son, K., 84-HYTASP-63 Song, H., 57-HYTASP-38, 75-HYTASP-55, 113-HYTASP-88 Song, W., 19-HYTASP-5, 42-HYTASP-26, 51-HYTASP-34, 68-HYTASP-48, 76-HYTASP-56 Staebler, T., 77-HYTASP-57 Steelant, J., 26-HYTASP-10, 85-HYTASP-64, 89-LEC-2, 106-HYTASP-82, 112-HYTASP-87, 118-HYTASP-93 Stella, F., 22-HYTASP-8 Su, B., 35-HYTASP-18 Su, E., 86-HYTASP-65, 113-HYTASP-88 Su, G., 102-HYTASP-78, 112-HYTASP-87 Su, L., 79-HYTASP-59 Sumanik, S., 113-HYTASP-88

Sun, B., 60-HYTASP-42, 70-HYTASP-50 70-HYTASP-50

Sun, D., 100-HYTASP-77, 122-HYTASP-99, 127-HYTASP-100

Sun, M., 15-HYTASP-1, 25-HYTASP-9, 27-HYTASP-11, 29-HYTASP-13, 33-HYTASP-17, 38-HYTASP-21, 58-HYTASP-39, 63-HYTASP-43, 66-HYTASP-46, 124-HYTASP-102 Sun, S., 85-HYTASP-64 Sun, X., 74-HYTASP-53 Sung, H., 48-HYTASP-31, 60-HYTASP-42 Swiergiel, N., 92-HYTASP-69 Taddeo, L., 22-HYTASP-8 Taguchi, H., 41-HYTASP-24 Talyzin, V., 19-HYTASP-5, 29-HYTASP-13, 88-HYTASP-68, 99-HYTASP-76, 108-HYTASP-84, 124-HYTASP-102 Tan, T., 98-HYTASP-75 Tan, W., 96-HYTASP-73 Tan, Y., 36-HYTASP-19, 82-HYTASP-61 Tang, G., 54-HYTASP-35 Tang, H., 83-HYTASP-62 Tang, S., 16-HYTASP-2, 65-HYTASP-45, 71-HYTASP-51,

85-HYTASP-64 Tang, W., 36-HYTASP-19, 37-HYTASP-20 Taylor, I., 116-HYTASP-91 Teng, J., 29-HYTASP-13, 56-HYTASP-37, 88-HYTASP-68 Tengji, L., 66-HYTASP-46 Thirumangalath, S., 20-HYTASP-6 Tian, Y., 78-HYTASP-58, 80-HYTASP-60 Tong, Z., 57-HYTASP-38 Toro, P., 20-HYTASP-6, 21-HYTASP-7 Toso, F., 56-HYTASP-37, 65-HYTASP-45 Tuttle, S., 45-HYTASP-28 Umapathy, N., 20-HYTASP-6 Van den Eynde, J., 106-HYTASP-82 van Kleef, A., 126-HYTASP-97 Veeraragavan, A., 110-HYTASP-86 Vennik, J., 45-HYTASP-28, 122-HYTASP-99 Verberne, C., 126-HYTASP-97 Verstraete, D., 55-HYTASP-36 Vigano’, D., 36-HYTASP-19 Vilela, R., 21-HYTASP-7 Viola, N., 96-HYTASP-73, 115-HYTASP-90, 126-HYTASP-97 Vlasenko, V., 88-HYTASP-68 Voevodenko, N., 75-HYTASP-55, 86-HYTASP-65, 97-HYTASP-74, 116-HYTASP-91 Voggenreiter, H., 77-HYTASP-57 Voloschenko, O., 88-HYTASP-68 von Wolfersdorf, J., 112-HYTASP-87 Wang, A., 103-HYTASP-79 Wang, B., 78-HYTASP-58, 88-HYTASP-68, 100-HYTASP-77, 108-HYTASP-84

Wang, C., 16-HYTASP-2, 51-HYTASP-34, 97-HYTASP-74 Wang, F., 18-HYTASP-4 Wang, G., 31-HYTASP-15, 106-HYTASP-82 Wang, H., 33-HYTASP-17, 49-HYTASP-32, 58-HYTASP-39, 63-HYTASP-43, 124-HYTASP-102 Wang, J., 35-HYTASP-18, 36-HYTASP-19, 44-HYTASP-27, 55-HYTASP-36, 69-HYTASP-49, 79-HYTASP-59, 87-HYTASP-66, 95-HYTASP-72Wang, K., 60-HYTASP-42 Wang, L., 25-HYTASP-9, 42-HYTASP-26, 83-HYTASP-62, 94-HYTASP-71, 125-HYTASP-103 Wang, P., 47-HYTASP-30 Wang, Q., 31-HYTASP-15 Wang, R., 75-HYTASP-55 Wang, S., 31-HYTASP-15, 54-HYTASP-35, 73-HYTASP-52, 87-HYTASP-66, 94-HYTASP-71 Wang, T., 59-HYTASP-40, 113-HYTASP-88, 118-HYTASP-93 Wang, W., 75-HYTASP-55 Wang, X., 15-HYTASP-1, 22-HYTASP-8, 125-HYTASP-103 Wang, Y., 19-HYTASP-5, 28-HYTASP-12, 30-HYTASP-14, 31-HYTASP-15, 42-HYTASP-26, 47-HYTASP-30, 49-HYTASP-32, 57-HYTASP-38, 60-HYTASP-42, 70-HYTASP-50, 71-HYTASP-51, 74-HYTASP-53, 75-HYTASP-55, 76-HYTASP-56, 77-HYTASP-57, 86-HYTASP-65, 104-HYTASP-80, 105-HYTASP-81, 119-HYTASP-94, 124-HYTASP-102, 127-HYTASP-100 Wang, Z., 21-HYTASP-7, 26-HYTASP-10, 27-HYTASP-11, 29-HYTASP-13, 33-HYTASP-17, 63-HYTASP-43, 66-HYTASP-46, 70-HYTASP-50, 74-HYTASP-53, 78-HYTASP-58, 124-HYTASP-102, 126-HYTASP-97 Wartemann, V., 15-HYTASP-1, 25-HYTASP-9, 65-HYTASP-45 Watanabe, K., 41-HYTASP-24 Wei, B., 98-HYTASP-75, 110-HYTASP-86 Wei, C., 73-HYTASP-52, 86-HYTASP-65, 115-HYTASP-90 Wei, D., 41-HYTASP-24 Wei, L., 83-HYTASP-62 Wei, X., 57-HYTASP-38, 67-HYTASP-47, 87-HYTASP-66, 124-HYTASP-102 Wei, Z., 86-HYTASP-65 Weihs, H., 65-HYTASP-45 Wen, C., 16-HYTASP-2 Wenbo, M., 45-HYTASP-28 Wenkai, W., 32-HYTASP-16, 35-HYTASP-18 Wenli, Z., 20-HYTASP-6 Wenxing, F., 28-HYTASP-12 Wenxiong, X., 20-HYTASP-6 West, T., 105-HYTASP-81

Wheatley, V., 110-HYTASP-86 Wilson, D., 40-HYTASP-23, 107-HYTASP-83 Wittal, M., 15-HYTASP-1 Wu, C., 22-HYTASP-8 Wu, F., 70-HYTASP-50 Wu, H., 28-HYTASP-12, 47-HYTASP-30 Wu, J., 21-HYTASP-7, 22-HYTASP-8, 47-HYTASP-30, 76-HYTASP-56 Wu, K., 87-HYTASP-66 Wu, L., 48-HYTASP-31, 119-HYTASP-94 Wu, R., 86-HYTASP-65 Wu, S., 73-HYTASP-52 Wu, X., 18-HYTASP-4, 19-HYTASP-5 Wu, Y., 57-HYTASP-38, 69-HYTASP-49, 75-HYTASP-55, 77-HYTASP-57, 96-HYTASP-73, 113-HYTASP-88, 118-HYTASP-93 Wu, Z., 77-HYTASP-57, 103-HYTASP-79 Xia, C., 99-HYTASP-76, 118-HYTASP-93 Xia, G., 58-HYTASP-39 Xiang, X., 49-HYTASP-32 Xianhong, X., 17-HYTASP-3 Xiao, B., 80-HYTASP-60 Xiao, F., 25-HYTASP-9 Xiao, G., 41-HYTASP-24 Xiao, X., 66-HYTASP-46 Xiao, Y., 37-HYTASP-20 Xiao, Z., 113-HYTASP-88, 122-HYTASP-99 Xiaobin, X., 66-HYTASP-46 Xiaopeng, Z., 126-HYTASP-97 Xie, A., 21-HYTASP-7 Xie, B., 68-HYTASP-48 Xie, F., 85-HYTASP-64 Xie, L., 97-HYTASP-74, 107-HYTASP-83 Xin, J., 32-HYTASP-16, 41-HYTASP-24, 50-HYTASP-33 Xin, R., 48-HYTASP-31 Xing, F., 20-HYTASP-6, 30-HYTASP-14, 40-HYTASP-23, 67-HYTASP-47, 125-HYTASP-103 Xing, J., 80-HYTASP-60 Xinguo, L., 17-HYTASP-3 Xinyu, C., 125-HYTASP-103 Xiong, P., 33-HYTASP-17 Xiong, Y., 56-HYTASP-37, 65-HYTASP-45 Xu, B., 125-HYTASP-103 Xu, D., 36-HYTASP-19 Xu, H., 18-HYTASP-4, 29-HYTASP-13 Xu, J., 25-HYTASP-9, 46-HYTASP-29, 82-HYTASP-61, 119-HYTASP-94, 120-HYTASP-95, 125-HYTASP-103 Xu, K., 54-HYTASP-35, 63-HYTASP-43 Xu, L., 95-HYTASP-72 Xu, M., 44-HYTASP-27

127-HYTASP-100

Siebenhaar,A., 2-PLNRY-1, 5-PLNRY-4, 7-PLNRY-5, 9-PLNRY-6, 11-LEC-1

Sun, L., 47-HYTASP-30, 96-HYTASP-73

Author/Session Chair IndexXu, S., 70-HYTASP-50 Xu, W., 39-HYTASP-22 Xu, X., 41-HYTASP-24 Xu, Y., 46-HYTASP-29, 85-HYTASP-64, 105-HYTASP-81 Xu, Z., 28-HYTASP-12, 65-HYTASP-45 Xuan, J., 19-HYTASP-5 Xue, L., 51-HYTASP-34 Xue, Y., 83-HYTASP-62 Ya, Y., 105-HYTASP-81 Yachao, L., 127-HYTASP-100

Yan, Z., 95-HYTASP-72, 104-HYTASP-80,

114-HYTASP-89

Yan, B., 28-HYTASP-12 Yan, C., 44-HYTASP-27 Yan, D., 67-HYTASP-47 Yan, G., 124-HYTASP-102 Yan, H., 18-HYTASP-4, 28-HYTASP-12, 63-HYTASP-43,

77-HYTASP-57 Yan, L., 126-HYTASP-97 Yan, X., 55-HYTASP-36, 64-HYTASP-44, 66-HYTASP-46, 75-HYTASP-55, 86-HYTASP-65

Yang, H., 29-HYTASP-13 Yang, J., 32-HYTASP-16, 42-HYTASP-26,

84-HYTASP-63, 88-HYTASP-68, 100-HYTASP-77, 102-HYTASP-78, 109-HYTASP-85, 112-HYTASP-87, 127-HYTASP-100 Yang, L., 55-HYTASP-36, 77-HYTASP-57, 99-HYTASP-76 Yang, S., 80-HYTASP-60, 88-HYTASP-68, 109-HYTASP-85 Yang, T., 16-HYTASP-2 Yang, W., 67-HYTASP-47 Yang, X., 36-HYTASP-19, 41-HYTASP-24 Yang, Y., 28-HYTASP-12, 54-HYTASP-35, 63-HYTASP-43, 73-HYTASP-52, 82-HYTASP-61, 97-HYTASP-74 Yang, Z., 27-HYTASP-11 Yanji, H., 20-HYTASP-6 Yao, J., 32-HYTASP-16, 41-HYTASP-24 Yao, W., 35-HYTASP-18, 44-HYTASP-27, 73-HYTASP-52, 87-HYTASP-66, 127-HYTASP-100 Yao, X., 46-HYTASP-29, 85-HYTASP-64 Yao, Y., 20-HYTASP-6 Ye, J., 31-HYTASP-15 Ye, Z., 29-HYTASP-13 Yi, M., 94-HYTASP-71 Yi, S., 82-HYTASP-61 Yin, G., 82-HYTASP-61 Yin, X., 57-HYTASP-38 Yin, Y., 45-HYTASP-28

Yin, Z., 30-HYTASP-14, 106-HYTASP-82 Yinan, J., 125-HYTASP-103 Ying, W., 122-HYTASP-99 Yingchuan, W., 42-HYTASP-26, 100-HYTASP-77, 109-HYTASP-85 Yong, E., 17-HYTASP-3 Yongchao, W., 18-HYTASP-4 You, J., 109-HYTASP-85 You, Y., 2-LEC-1, 3-PLNRY-2, 4-PLNRY-3,


116-HYTASP-91, 125-HYTASP-103, 128-PANEL-3 Yu, A., 42-HYTASP-26, 100-HYTASP-77, 109-HYTASP-85, 118-HYTASP-93, 125-HYTASP-103 Yu, C., 84-HYTASP-63 Yu, D., 54-HYTASP-35 Yu, H., 107-HYTASP-83 Yu, J., 45-HYTASP-28, 60-HYTASP-42, 65-HYTASP-45,

102-HYTASP-78,

Yu, M., 64-HYTASP-44 Yu, X., 21-HYTASP-7, 119-HYTASP-94 Yu, Y., 18-HYTASP-4, 99-HYTASP-76 Yu, Z., 38-HYTASP-21, 85-HYTASP-64 Yuan, H., 19-HYTASP-5, 71-HYTASP-51, 118-HYTASP-93 Yuan, J., 37-HYTASP-20 Yuan, L., 17-HYTASP-3, 30-HYTASP-14 Yuan, T., 19-HYTASP-5 Yuan, X., 64-HYTASP-44 Yuan, Y., 44-HYTASP-27 Yuanyuan, H., 68-HYTASP-48 Yue, C., 64-HYTASP-44 Yue, L., 42-HYTASP-26, 51-HYTASP-34 Yueyong, L., 75-HYTASP-55 Zakharov, V., 35-HYTASP-18, 44-HYTASP-27 Zeng, H., 21-HYTASP-7 Zeng, J., 77-HYTASP-57 Zeng, L., 64-HYTASP-44, 112-HYTASP-87 Zeng, M., 36-HYTASP-19, 104-HYTASP-80 Zeng, S., 44-HYTASP-27 Zhan, D., 42-HYTASP-26, 109-HYTASP-85 Zhang, B., 102-HYTASP-78, 112-HYTASP-87 Zhang, C., 119-HYTASP-94 Zhang, D., 18-HYTASP-4, 29-HYTASP-13, 51-HYTASP-34 Zhang, E., 109-HYTASP-85 Zhang, G., 64-HYTASP-44 Zhang, H., 25-HYTASP-9, 30-HYTASP-14, 66-HYTASP-46, 78-HYTASP-58, 96-HYTASP-73, 105-HYTASP-81, 107-HYTASP-83, 112-HYTASP-87

Zhang, J., 25-HYTASP-9, 55-HYTASP-36, 60-HYTASP-42,

Zhang, K., 22-HYTASP-8, 32-HYTASP-16, 33-HYTASP-17, 47-HYTASP-30, 70-HYTASP-50, 100-HYTASP-77, 119-HYTASP-94 Zhang, L., 33-HYTASP-17, 86-HYTASP-65, 87-HYTASP-66, 105-HYTASP-81 Zhang, P., 79-HYTASP-59, 87-HYTASP-66 Zhang, Q., 60-HYTASP-42, 119-HYTASP-94 Zhang, R., 15-HYTASP-1, 57-HYTASP-38 Zhang, S., 18-HYTASP-4, 78-HYTASP-58, 87-HYTASP-66 Zhang, T., 22-HYTASP-8, 126-HYTASP-97 Zhang, W., 30-HYTASP-14 Zhang, X., 15-HYTASP-1, 42-HYTASP-26, 78-HYTASP-58, 104-HYTASP-80 Zhang, Y., 25-HYTASP-9, 33-HYTASP-17, 37-HYTASP-20, 46-HYTASP-29, 68-HYTASP-48, 78-HYTASP-58, 84-HYTASP-63, 98-HYTASP-75, 116-HYTASP-91, 124-HYTASP-102 Zhang, Z., 31-HYTASP-15, 37-HYTASP-20, 57-HYTASP-38 Zhao, D., 70-HYTASP-50 Zhao, G., 63-HYTASP-43 Zhao, H., 94-HYTASP-71 Zhao, J., 51-HYTASP-34 Zhao, L., 96-HYTASP-73 Zhao, M., 40-HYTASP-23 Zhao, R., 44-HYTASP-27 Zhao, W., 31-HYTASP-15, 82-HYTASP-61, 87-HYTASP-66, 97-HYTASP-74, 110-HYTASP-86Zhao, Y., 19-HYTASP-5, 29-HYTASP-13, 60-HYTASP-42, 82-HYTASP-61, 103-HYTASP-79, 104-HYTASP-80, 106-HYTASP-82 Zhao, Z., 54-HYTASP-35 Zhen, H., 54-HYTASP-35 Zheng, H., 18-HYTASP-4 Zheng, J., 30-HYTASP-14 Zheng, R., 21-HYTASP-7, 79-HYTASP-59, 96-HYTASP-73, 105-HYTASP-81 Zheng, S., 15-HYTASP-1, 78-HYTASP-58 Zheng, W., 44-HYTASP-27, 54-HYTASP-35 Zheng, X., 56-HYTASP-37 Zheng, Z., 94-HYTASP-71 Zhengze, Z., 124-HYTASP-102 Zhirnov, D., 59-HYTASP-40 Zhong, F., 78-HYTASP-58, 94-HYTASP-71, 122-HYTASP-99 Zhong, S., 37-HYTASP-20 Zhong, Z., 58-HYTASP-39

Zhongyan, Y., 56-HYTASP-37 Zhou, H., 54-HYTASP-35 Zhou, J., 96-HYTASP-73 Zhou, L., 44-HYTASP-27 Zhou, W., 97-HYTASP-74 Zhou, X., 29-HYTASP-13, 88-HYTASP-68 Zhou, Z., 60-HYTASP-42, 83-HYTASP-62 Zhu, B., 32-HYTASP-16 Zhu, C., 33-HYTASP-17, 73-HYTASP-52, 83-HYTASP-62, 116-HYTASP-91, 125-HYTASP-103 Zhu, G., 69-HYTASP-49 Zhu, J., 40-HYTASP-23, 55-HYTASP-36, 113-HYTASP-88 Zhu, K., 27-HYTASP-11, 38-HYTASP-21, 66-HYTASP-46 Zhu, S., 79-HYTASP-59, 125-HYTASP-103 Zhu, W., 32-HYTASP-16, 125-HYTASP-103 Zhu, Y., 20-HYTASP-6, 22-HYTASP-8, 84-HYTASP-63 Zhuo, C., 70-HYTASP-50 Zou, Z., 93-HYTASP-70, 118-HYTASP-93 Zuo, G., 26-HYTASP-10, 127-HYTASP-100


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