resume of william s. saric 1 education ...kswt.tamu.edu/files/resumes/ws_resume.pdfresume of william...

RESUME OF WILLIAM S. SARIC

1 EDUCATION & REGISTRATION 2

2 EXPERIENCE 2

3 CONSULTING 3

4 PROFESSIONAL HONORS AND ACTIVITIES 3

5 TEACHING 4

6 SCHOLARLY AND CREATIVE CONTRIBUTIONS 9

Publications – Journal and Society Papers 9

Publications – Editor 14

Publications – Technical Reports 14

Talks and Lectures 15

7 MAJOR PROJECTS AT TEXAS A&M UNVERSITY 24

8 ASU WIND TUNNEL PROJECTS 25

9 SPONSORED RESEARCH ACTIVITIES 25

Texas A&M University 25

Arizona State University 26

Virginia Polytechnic Institute & State University 28

Résumé of W. S. Saric page 2

WILLIAM S. SARIC, P.E. Stewart & Stevenson Services Inc. Professor, Department of Aerospace Engineering

Texas A&M University College Station TX 77843-3141

[email protected]

1 EDUCATION & REGISTRATION

B.S. in Mechanical Engineering, January 1963, Illinois Institute of Technology, Chicago, Illinois. Pi Tau Sigma Outstanding Mechanical Engineering Graduate of his class. Thesis: "Design, Construction and Performance of a Dynamic Balancing Machine," Advisor - Dr. R.J. Bonthron.

M.S. in Mechanical Engineering, June 1965, University of New Mexico (thesis not required).

Ph.D. in Mechanics, June 1968, Illinois Institute of Technology, Chicago, Illinois. Thesis: "The Hydrodynamic Stability of Heterogeneous Couette Flows." Advisor - Dr. Zalman Lavan.

P.E. Registered Professional Engineer in Virginia, Lic. No. 13427.

2 EXPERIENCE

January 2005 - Present: Texas A&M University, Stewart & Stevenson Services Inc. Professor, Aerospace Engineering. Supervisor: Dean John Niedzwecki. Duties include teaching, research, and student advisement.

August 1984 – December 2004: Arizona State University, Professor, Mechanical and Aerospace Engineering. Chairman: Dr. Robert Peck. Duties include teaching, research, and student advisement.

Jan 2000 – Nov 2000: Arizona State, Vice Chair Aerospace Engineering. Duties included responsibility for ABET accreditation visit and supervision of the undergraduate curriculum in Aerospace Engineering.

Sep 1991 - Jul 1992: Tohoku University, Sendai, Japan, Professor, Aeronautics & Astronautics. Duties included teaching, research and student advisement.

September 1975 - August 1984: Virginia Polytechnic Institute and State University, Professor, Engineering Science and Mechanics. Chairman: Dr. D. Frederick. Duties included teaching, research, and student advisement. Tenure awarded, May 1978. Promoted from Associate Professor to Professor, May 1979.

July 1968 - August 1975: Sandia National Laboratories, Albuquerque, Staff Member, Atomic and Fluid Physics Division. Manager: Dr. K.J. Touryan. Duties included research and advising the Aerodynamics Projects group on problems of reentry ablation studies, boundary-layer transition, transpiration cooling, heat transfer, and applied mathematics. Research projects included experimental and theoretical studies in liquid-layer stability, boundary-layer stability, explosive welding, nonlinear dynamics, nonlinear oscillations of bubbles, and stability of controlled fusion of deuterium-tritium with electron beams.

January 1966 - June 1968: Illinois Institute of Technology, Full-time Instructor, Mechanics Department. Chairman: Dr. P. Chiarulli. Duties involved teaching undergraduate Mechanics courses, textbook review and selection, course organization, and supervision of a graduate teaching assistant.

January 1963 - January 1966: Sandia National Laboratories, Albuquerque, Staff Member. Supervisors: H.D. Sivinski and K.J. Touryan. Worked in environmental testing organization for two years on high-velocity impact. Duties involved feasibility studies and design of simulation facilities for various environments and writing budget proposals for new facilities. One year in Reentry Vehicle Research Division working on Magnetohydrodynamic entrance flows and high-speed boundary-layer flows.

Summer 1962: Illinois Institute of Technology, NSF Undergraduate Research Fellow. Supervisor: Dr. R.J. Bonthron. Worked on undergraduate thesis.

March 1958 - October 1960: Dewey and Almy Chemical Company of W.R. Grace, Chicago, Illinois, Chemical Mixer. Duties included responsibility of second-shift production of concrete admixture products.


3 CONSULTING

May 2002 – present: Northrop-Grumman Corp. Consulted on problems of laminarization for SensorCraft.

May 1984 - June 1985: Lawrence Livermore National Laboratories. Consulted on problems of Atomic Vapor Laser Isotope Separation and gas centrifuge isotope separation.

January 1977 - June 1986: Lockheed-Georgia, Marietta, Georgia. Consulted on problems of laminarization of flow over airfoils for subsonic transports and on experiments on boundary-layer stability.

September 1975 - 1987: Sandia National Laboratories, Albuquerque. Conducted research on the stability of controlled nuclear controlled nuclear fusion, magnetohydrodynamic power generation, convection in porous media, reactor safety problems, and hypersonic boundary-layer transition.

4 PROFESSIONAL HONORS AND ACTIVITIES

Scientific and Professional Societies

Fellow, American Physical Society (APS) 1982 Life Fellow, American Society of Mechanical Engineers (ASME) 1993 Fellow, Amer. Inst. of Aeronautics and Astronautics (AIAA) 2005 Tau Beta Pi (Honorary) Pi Tau Sigma (Honorary)

Professional Recognition, Honors, and Service to the Profession

Member, National Academy of Engineering 2006.

Member, The Academy of Medicine, Engineering, and Science of Texas 2006.

Recipient of the MMAE Department, IIT Alumni Recognition Award 2005.

Recipient of the AIAA Fluid Dynamics Award 2003.

Recipient of the AGARD (NATO) Scientific Achievement Award 1996.

Recipient of the G. I. Taylor Medal from the Society of Engineering Science, June 1993.

Recipient of VPI & SU 1984 Alumni Award for Research Excellence for "...contributions to the understanding of nonlinear flow stability and subharmonic transition to turbulence."

Winner of Gallery of Fluid Motions Prize "...for visualization of different transition mechanisms," at the 26th Annual Meeting of the APS Division of Fluid Dynamics, November 1983.

Awarded Certificate of Teaching Excellence, VPI & SU, 1978.

Invited guest of the U.S.S.R. Academy of Sciences (3 times), Jun 8 - Jul 6, 1976; Sep 2 - 10, 1979; August 16, - Sep 6, 1981. Gave lectures and toured facilities at the Institute of Theoretical and Applied Mechanics, Institute of Hydrodynamics, and the Institute of Thermal Physics in Akademgorodok/Novosibirsk and at the Moscow State University and the Center for Computing in Moscow. Worked on joint wind-tunnel experiments at the Institute of Theoretical and Applied Mechanics.

Fellow, Japan Society for the Promotion of Science. Gave a series of lectures in Japan during Sep / Oct 1989.

Aerospace Engineering Evaluator for ABET, 2000-2004.

Associate Editor, Physics of Fluids, 1998-2000

Associate Editor, Applied Mechanics Review, 1984-1994

Associate Editor, J. Fluids Engineering, 1993-1996.

Associate Editor, J. Applied Mechanics, 2000-2003.

Member of AGARD Fluid Dynamics Panel, 1989-1994.


Member of AIAA Technical Committee on Fluid Dynamics and the Fluids Liaison to the AIAA Technical Committee on Plasma Dynamics, 1975-1978.

Chairman, U.S. Boundary-Layer Transition Study Group, 2001-present, member since 1981. Now a Working Group of the AIAA Fluid Dynamics TC.

Member of AIAA Technical Committee on Ground Testing, 1983-1986

General Chairman, AIAA 11th Fluid and Plasma Dynamics Conference, Seattle, Washington, Jul 10-12, 1978. With 115 papers presented and 280 attendees, responsibilities included organizing the technical committee, paper review, session topics, invited papers, etc.

Chairman, ASME Applied Mechanics Division, 1991/1992. Member, Executive Committee, 1986-1992.

Chairman, Fluid Mechanics Technical Committee, ASME Applied Mechanics Division, 1984 - 1987 (member, 1982-1984).

Vice Chairman, Executive Committee, APS Division of Fluid Dynamics, 1985-1986.

Member of SAE Technical Committee on Aerodynamics, 1984-1991.

Member of National Academy of Sciences, National Research Council, Aerodynamics Panel for the NRC Workshop on Aeronautical Technology in the Year 2000. University of Texas, Austin, Jan 16-19, 1984.

Member of Scientific Committee of the 2nd IUTAM Symposium on Laminar-Turbulent Transition, Jul 9-13, 1984, Novosibirsk, U.S.S.R.; 3rd IUTAM Symposium on Laminar-Turbulent Transition, Toulouse, France, Sep 11-15, 1989; 4th IUTAM Symposium on Laminar-Turbulent Transition, Sendai, Japan, Sep. 5-9, 1994; 6th IUTAM Symposium on Laminar Turbulent Transition, Bangalore, India, Dec. 6-10, 2004.

Chairman and Organizer of the 5th IUTAM Symposium on Laminar-Turbulent Transition, Sep 13-17, 1999, Sedona Arizona.

Member of Steering Committee of NSF Engineering Fluid Mechanics Workshop, Sep 17-20, 1986.

Co-chairman of Symposium Use of Artificial Excitation to Control Fluid Flows by Manipulating Their Large-Scale Structure, ASME Applied Mechanics Conference, San Antonio, Jun 17-21, 1984.

Co-chairman of Symposium Stability and Convection, ASME 106th Winter Annual Meeting, Miami Beach, Nov 17-21, 1985.

Co-Chairman of International Workshop on Stability and Transition in Bounded Shear Flows, Tucson, Arizona, Nov 22-23, 1985.

Co-Chairman of International Workshop on Dynamics of Structure and Intermittencies in Turbulence, Tempe, Arizona, May 20-24, 1991.

Chairman of 45 technical sessions at National and International Meetings.

Listed: Who's Who in Aviation and Aerospace: 1st Edition (U.S.) 1983.

Listed: American Men and Women in Science, 1982.

Current Fields of Interest

Wind-tunnel and flight experiments in the areas of boundary-layer stability and transition, laminar flow control, and low-Reynolds-number aerodynamics. Theoretical and computational studies in hydrodynamic stability, nonlinear waves, stratified fluids, and Taylor-Görtler vortices. Flight measurements of air quality.

5 TEACHING

Texas A&M University

Ph.D. Students Supervised

A.L. Carpenter, in progress


L. Hunt, in progress

C. Kluzek, in progress

J. Hofferth, in progress

M.S. Students Supervised

S. Schouten, in progress

C.W. McKnight, 2006 “Design and Safety Analysis of In-Flight, Laminar Flow Control, Airfoil,” Aug 2006.

Arizona State University

Post-Doc and Visiting Scientists

Dr. Shohei Takagi, National Aerospace Laboratories, Tokyo, Japan, Nov 1985-Oct 1987 and Jan-Mar 1991.

J.R. Dagenhart, NASA-Langley Research Center, "Thompson Fellow," Aug 1986-Aug 1987.

Dr. Yasuaki Kohama, Tohoku University, Sendai, Japan, Oct 1989-Aug 1990.

Dr. Vladimir Kosorygin, Institute of Theoretical and Applied Mechanics, USSR Academy of Sciences, Novosibirsk, Sept 1990-May 1991.

Dr. Vsevolod Shidlovskii, Computing Center, USSR Academy of Sciences, Moscow, Mar-Apr 1991.

Dr. Sandrine Jarre, IMST, University Marseille-Aix Provence II, Marseille, France, Sep 1994 - Sep 1995.

Dr. Nina Yurchenko, Hydromechanics Institute, Ukranian Academy of Sciences, Kiev, Oct-Dec 1996.

Dr. Mark Reibert, Motorola, Scottsdale, AZ, Aug 1996 – Aug 1997.

Dr. Keith Chapman, Fender Guitar Co., Scottsdale, AZ, Jan 1997 – Jun 1998

Dr. Ronald Radeztsky, Motorola, Scottsdale, AZ, Sep 1998 – Sep 1999.

Dr. Simone Zuccher, Politecnico di Milano, Italia, Feb 2002 – Feb 2004.


J.R. Dagenhart, 1992. "Crossflow Stability and Transition Experiments on a Swept Wing," Dec 1992 (VPI & SU).

A. Benmalek, 1993. "Nonlinear Development of Görtler Vortices over Variable Curvature Walls," May 1993.

R.H. Radeztsky, Jr. 1994. "Growth and Development of Roughness-Induced Stationary Crossflow Vortices," Mar 1994.

M.S. Reibert, 1996. "Nonlinear Stability, Saturation, and Transition in Crossflow-Dominated Boundary Layers" May 1996.

E.B. White, 2000. “Secondary instability in three-dimensional boundary layers.” Aug 2000

J. Montinnen, 2004. “Computational study of the effect of winglets on the performance of micro-aerial vehicles.”


M.C. Mousseux, 1988. "Flow Quality Improvements in the ASU Unsteady Wind Tunnel," Aug 1988.

P.T. Pupator, 1988. "Control of Random Two-Dimensional Disturbances in a Boundary Layer," Dec 1988.

J.A. Hoos, 1990. "Boundary-Layer Receptivity To Freestream Sound," May 1990.

S.A. Spencer, 1992. "Boundary-Layer Receptivity To Freestream Sound and 3-D Roughness Elements," May 1992.


B.K. Rasmussen, 1993. "Boundary Layer Receptivity - Freestream Sound on an Elliptical Leading Edge," May 1993.

W. Wei, 1994. "Boundary-Layer Receptivity: Freestream Sound on a 20:1 Elliptical Leading Edge,” August 1994.

G. Höhne, 1996. "Flow Uniformity Measurements over Porous Suction Panels," June 1996 (Diplomarbeit, Technische Universität Berlin).

J. Buxbaum, 1996. "Flow Uniformity Measurements over Porous Suction Panels," June 1996 (Diplomarbeit, Technische Universität Berlin).

T.K. Krutckoff, 1996. "Experiments on Boundary-Layer Receptivity to Sound," Aug 1996.

R. Carrillo, 1996. “Distributed-Roughness Effects on Stability and Transition in Swept-Wing Boundary Layers,” Dec. 1996.

P. Gabet, 2001. “Pulsed sound techniques for leading edge receptivity.” Dec 2001.

R. Gladden, 2001. “Role of random distributed roughness on boundary layer transition.” Dec 2001.

C. Kang, 2001. “The Use of InfraRed Thermography in Transition Detection on Swept Wings at Mach 2.4.” Dec 2001. (Diplomarbeit, Technical University of Delft).

B. Latek, 2001. “Experiments on low-Reynolds-number aerodynamics for micro aerial vehicles.” May 2001

Senior Projects Supervised

J. Bellis, "Design of a Wind-Tunnel Test Section," Dec 1984.

T. Chesebrough, "Design of a Three-Dimensional Hot-Wire Positioning Device," Dec 1984.

T. Grochowski, "Software Design for Wind Tunnel Data Acquisition System," Dec 1985.

L. Rottman, "3-D Graphics Interface on a Tektronix Plotter Using a PC," Dec 1985.

J. Frazier, "Measurement of Drag in the Aerodynamic Wind Tunnel," May 1987.

B. Yonkovich, "Wind Tunnel Test-Section Design," May 1987.

C. Kaus, "3-D Traverse Design," Dec 1987.

D. Grady, "Design of a Wind Tunnel Heat Exchanger," Dec 1988.

T. Hendricks and P. Simonich, "Design of a Turning Vane Heat Exchanger," May 1989.

M. Gersten, "Design of Special Optics for a Laser-Doppler Anemometer," Aug 1989.

T. Krutckoff, "Visualization of Low-Reynolds-Number Flow Fields Around Two-Dimensional Roughness Elements," (Honors Thesis) Dec 1991.

T. Takeuchi, “Flow Visualization Wind Tunnel-Smoke Insertion Traverse Design,” Dec. 1994.

T. Silverman “Design and safety analysis of a model mounting structure for the Cessna O-2 aircraft,” May 2005.

M. Belisle “Experiments on a modulated Taylor-Couette flow,” Dec. 2005.

S. Benyi “Hotwire calibration at variable Mach number and variable total pressure,” May 2006.

Virginia Polytechnic Institute and State University

General

Adjunct Professor, 1974 Academic Year


Group leader for 29 engineering students on a two-week tour of the U.S.S.R., Mar 1979. Also organized the scientific and educational visits to the Academy of Science Computing Center, Moscow State University, and Latvian State University.

Served on 15 Ph.D. Committees and 8 M.S. Committees.


J. Floryan, "Stability of Boundary-Layer Flows over Curved Surfaces," Jan 1980.

G. Reynolds, "Experiments on the Stability of a Flat-Plate Boundary Layer with Suction," Jan 1982.


G. Reynolds, "Experiments on the Stability of Boundary-Layer Flows," May 1979.

G. Tice, "Experimental Investigation on the Stability of Taylor-Couette Flow," Dec 1981.

C. Costis, "Excitation of Wave Packets and Random Disturbances in a Boundary Layer," May 1982.

L. Yeates, "The Three-Dimensional Flow Field Over Swept-Leading-Edge Models," Sep 1984.

J. Crouch, "A Flying Hot-Wire Study of Separation over a FX-63-137 Airfoil," Jul 1985.

Senior Projects Supervised

W. Cousins, "Design and Construction of a 3-D Traverse Mechanism for Wind Tunnels," Mar 1978.

R. Gram, "Design of a Boundary-Layer Suction Device for Laminar Flow Control," Jun 1978.

L. Peach, "Airfoil Design for Man-Powered Aircraft," Jun 1978.

T. Burton, "A Digital Control and Servo for a Three-Dimensional Traverse Mechanism," May 1980.

B. Spigel, "The Design and Construction of Wall Bumps for the 3-D Flow over a Flat Plate," May 1980.

M. Holland, "The Design and Construction of a Taylor Vortex Apparatus," May 1981.

T. Shanahan, "Comparison of Techniques Used for Drag Measurement on Automobiles," May 1981.

R. Williams, "A Design of a Lightweight Test Section for the VPI Stability Tunnel," May 1981.

C. Harvey, "Design of a Versatile Test Section for the VPI & SU Stability Tunnel," May 1983.

R. Henk, "Computer Controlled Wind-Tunnel Experiment," May 1983. Recipient of the D.H. Pletta Award for the outstanding senior project.

C. May, "A Panel-Method Code to Design Wind-Tunnel Modifications for Pressure Gradients on Models," May 1983. Runner-up for the D.H. Pletta Award for the outstanding senior project.

J. Carter, "A Lagrangian Code for Streakline Calculations," Jun 1984.

G. Rose, "Use of Piezoelectric Polymer Films to Detect Transition to Turbulence," Jun 1984.

J. McCay, "Design of a Hot-Wire Traverse Mechanism to Operate in High Dynamic Pressure, Cryogenic Environments," Aug 1984.


Sandia National Laboratories

Taught graduate level courses to the technical staff on "Hydrodynamic Stability" and "Perturbation Methods" as part of noon-hour educational program, Spring and Fall 1970.

Developed and taught an intensive (45 hours), 3-week course on "Perturbation Methods" to the technical staff in Albuquerque and to the technical staffs of Sandia Labs and Lawrence Livermore Labs in Livermore, California, Spring and Summer 1974.

Supervised experimental Ph.D. thesis of B. Marshall conducted at Sandia while Marshall was a student at Oklahoma State University.

University of New Mexico

Adjunct Professor, 1972. Course Taught: ME 504 Heat Conduction

Illinois Institute of Technology

Had responsibility for teaching large (greater than 100 students) sections of the Engineering Science Curriculum. Taught: ES 202 Statics and Dynamics, ES 203 Strength of Materials, and ES 204 Fluid Mechanics.


6 SCHOLARLY AND CREATIVE CONTRIBUTIONS

Publications - Journal and Society Papers

1. Saric, W.S. and Touryan, K.J. 1969 Incompressible Magnetohydrodynamic Entrance Flow in a Plane Channel. Phys. Fluids Vol. 12, pp 1412-1419.

2. Nayfeh, A.H. and Saric, W.S. 1971 Nonlinear Resonances in the Motion of Rolling Reentry Bodies. AIAA Paper No. 71-0047.

3. Nayfeh, A.H. and Saric, W.S. 1971 Nonlinear Kelvin-Helmholtz Instability. J. Fluid Mech. Vol. 46, pp 209-232

4. Saric, W.S. and Lavan, Z. 1971 Stability of Circular Couette Flow of Binary Mixtures. J. Fluid Mech. Vol. 47, pp 65-80.

5. Nayfeh, A.H. and Saric, W.S. 1971 Stability of a Fluid Film. AIAA J. Vol. 9, pp 750-752.

6. Saric, W.S. and Marshall, B.W. 1971 An Experimental Investigation of the Stability of a Thin Liquid Layer Adjacent to a Supersonic Stream. AIAA J. Vol. 9, pp 1546-1553.

7. Nayfeh, A.H., Saric, W.S. and Rodriquez, D. 1972 Surge Waves in Stranded Springs. J. of Engr. for Industry Vol. 94, Series B, pp 942-948.

8. Nayfeh, A.H. and Saric, W.S. 1972 An Analysis of a Asymmetric Rolling Bodies with Nonlinear Aerodynamics. AIAA J. Vol. 10, pp 1004-1022.

9. Nayfeh, A.H. and Saric, W.S. 1972 Nonlinear Waves in a Kelvin-Helmholtz Flow. J. Fluid Mech. Vol. 55, pp 311-327.

10. Nayfeh, A.H. and. Saric, W.S. 1973 Nonlinear Stability of a Liquid Film Adjacent to a Supersonic Stream. J. Fluid Mech. Vol. 53, pp 39-51.

11. Nayfeh, A.H. and Saric, W.S. 1974 Nonlinear Acoustic Response of a Spherical Bubble. J. of Sound and Vibration. Vol. 30, pp 445-453.

12. Nayfeh, A.H., Saric, W.S, and Mook, D.T. 1974 Stability of Nonparallel Flows. Archives of Mechanics. Vol. 26, pp 401-406.

13. Bordner, G.L., Nayfeh, A.H. and Saric, W.S. 1975 Stability of Liquid Layers Adjacent to Compressible Streams. ZAMP. Vol. 26, pp 771-783.

14. Saric, W.S. and Nayfeh, A.H. 1975 Nonparallel Stability of Boundary-Layer Flows. Phys. Fluids Vol. 18, pp 945-950.

15. Lekoudis, S.G., Nayfeh, A.H. and Saric, W.S. 1976 Compressible Boundary Layers over Wavy Walls. Phys. Fluids Vol. 19, pp 514-519.

16. Saric, W.S., Nayfeh, A.H. and Lekoudis, S.G. 1976 Experiments on the Stability of Liquid Films Adjacent to Supersonic Boundary Layers. J. Fluid Mech. Vol. 77, pp 63-87.

17. Saric, W.S., Touryan, K.J. and. Scott, M.R. 1977 Stability of Slag in Turbulent MHD Boundary Layers. J. Energy (AIAA) Vol. 1, pp 108-114.

18. Lekoudis, S.G., Nayfeh, A.H. and Saric, W.S. 1977 Third-Order Resonant Wave Interactions. Phys. Fluids Vol. 11, pp 1793-1795.

19. Saric, W.S. and Nayfeh, A.H. 1977 Nonparallel Stability of Boundary Layers with Suction. AGARD Laminar-Turbulent Transition CP-224.

20. Saric, W.S. and Reynolds, G.A. 1980 Experiments on the Nonlinear Stability of Waves in a Boundary Layer. In: Laminar-Turbulent Transition, Springer-Verlag.

21. Dovgal, A.V., Kozlov, V.V., Nosyrev, I.P and Saric, W.S. 1981 On the Visualization of Stream Structures in a Boundary Layer. (in Russian) Publication No. 37-81 of USSR Acad. Sci., Sib. Div., I.T.A.M.


22. Floryan, J.M. and Saric, W.S. 1982 Stability of Görtler Vortices in Boundary Layers. AIAA J. Vol. 20, pp 316-324.

23. Lekoudis, S.G., Nayfeh, A.H. and Saric, W.S. 1982 Nonlinear Wave Interactions in Supersonic Wind-Generated Waves. Phys. Fluids Vol. 25, pp 1524-1531.

24. Floryan, J.M. and Saric, W.S. 1983 Effect of Suction on the Görtler Instability of Boundary Layers. AIAA J. Vol. 21, pp 1635-1639.

25. Dagenhart, J.R. and Saric, W.S. 1983 An Orthogonal Coordinate Grid Following the Three-Dimensional Viscous Flow Over a Concave Surface. Proceedings of Symposium on Grid Generation Techniques, ASME Fluids Engineering Conference.

26. Floryan, J.M. and Saric, W.S. 1984 Wavelength Selection and Growth of Görtler Vortices. AIAA J. Vol. 22, pp 1529-1538.

27. Saric, W.S., Kozlov, V.V. and Levchenko, V. Ya. 1984 Forced and Unforced Subharmonic Resonance in Boundary-Layer Transition. AIAA Paper No. 84-0007.

28. Saric, W.S. and Peterson, J.B. 1984 Design of High-Reynolds-Number Flat Plate Experiments in the NTF. AIAA Paper No. 84-0588.

29. Saric, W.S. and Yeates, L.G. 1984 Generation of Crossflow Vortices in a Three-Dimensional Flat-Plate Flow. Laminar-Turbulent Transition. Vol. II, V. Kozlov ed., Springer-Verlag.

30. Saric, W.S. and Thomas, A.S.W. 1984 Experiments on the Subharmonic Route to Transition. Turbulence and Chaotic Phenomena in Fluids. Ed: T. Tatsumi, North-Holland.

31. Kozlov, V.V., Levchenko, V. Ya. and Saric, W.S. 1984 Formation of Three-Dimensional Structure at Transition in a Boundary Layer. (in Russian) , Mekanika Zhidkosti i Gaza. No. 6, pp 42-50. (authors listed alphabetically).

32. Saric, W.S. and Yeates, L.G. 1985 Experiments on the Stability of Crossflow Vortices in Swept-Wing Flows. AIAA Paper No. 85-0493 .

33. Reynolds, G.A. and Saric, W.S. 1986 Experiments on the Stability of a Flat-Plate Boundary Layer with Suction. AIAA J. Vol. 24, pp 202-207.

34. Saric, W.S. and Reed, H.L. 1986 Effect of Suction and Mass Injection Boundary-Layer Transition. AIAA J. Vol. 24, pp. 383-389.

35. Crouch, J.D. and Saric, W.S. 1986 Oscillating Hot-Wire Measurements Above An FX63-137 Airfoil. AIAA Paper No. 86-0012.

36. Saric, W.S. 1986 Visualization of Different Transition Mechanisms. Phys. Fluids. Vol. 29, pp 2770.

37. Saric, W.S. 1986 Boundary Layer Transition to Turbulence: The last five years. Proc. 10th Symposium on Turbulence. University of Missouri-Rolla.

38. Saric, W.S. and Reed, H.L. 1987 Three-Dimensional Stability of Boundary Layers. Perspectives in Turbulence. Eds: U. Meier and P. Bradshaw, Springer-Verlag.

39. Saric, W.S., Takagi, S. and Mousseux, M.C. 1988 Fundamental Requirements for Freestream Turbulence Measurements. AIAA Paper No. 88-0053.

40. Reed, H.L. and Saric, W.S. 1989 Stability of Three-Dimensional Boundary Layers. Ann. Rev. Fluid Mech. Vol. 21, pp 235-284.

41. Saric, W.S., Dagenhart, J.R. and Mousseux, M.C. 1990 Experiments in Swept-Wing Transition. Numerical and Physical Aspects of Aerodynamic Flows. Vol. 4, Ed: T. Cebeci, Springer-Verlag.

42. Pupator, P.T. and Saric, W.S. 1989 Control of Random Disturbances in a Boundary Layer. AIAA Paper No. 89-1007.


43. Dagenhart, J.R., Saric, W.S., Mousseux, M.C. and Stack, J.P. 1989 Crossflow-Vortex Instability and Transition on a 45-Degree Swept Wing. AIAA Paper No. 89-1892.

44. Saric, W.S. 1989 Boundary Layer Stability and Transition. Proc. 5th International Conference on Numerical Ship Hydrodynamics. Hiroshima, Japan.

45. Dagenhart, J.R., Saric, W.S., Hoos, J.A. and Mousseux, M.C. 1990 Experiments on Swept-Wing Boundary Layers. Laminar-Turbulent Transition. Vol. III. eds. D. Arnal and R. Michel, Springer-Verlag.

46. Day, H.L., Herbert, T. and Saric, W.S. 1990 Comparison of Local and Marching Analyses of Görtler Instability. AIAA J. Vol. 28, pp 1010 - 1015.

47. Reed, H.L., Lin, N. and Saric, W.S. 1990 Boundary layer receptivity to sound: Navier-Stokes computations. Appl. Mech. Rev. Vol. 43, No. 5, Part 2, pp 175-180.

48. Mangalam, S.M., Maddalon, D.V., Saric, W.S. and Agarwal, N.K. 1990 Measurements of Crossflow Vortices, Attachment-Line Flow, and Transition Using Microthin Hot Films. AIAA Paper No. 90-1636.

49. Saric, W. S. 1990 Low-Speed Experiments: Requirements for Stability Measurements. Instability and Transition. Vol. I. Ed: Y. Hussaini, Springer-Verlag, pp 162 - 174.

50. Kohama, Y., Saric, W.S. and Hoos, J.A. 1991 A High Frequency Instability of Crossflow Vortices that leads to Transition. Proc. Roy. Aero. Soc.: Boundary-Layer Transition and Control, Cambridge.

51. Lin, N., Reed, H.L. and Saric, W.S. 1991 Leading-Edge Receptivity: Navier-Stokes Computations. Proc. Roy. Aero. Soc.: Boundary Layer Transition and Control, Cambridge.

52. Saric,W.S. and Benmalek, A. 1991 Görtler Vortices With Periodic Curvature. Proc. ASME-FED Vol. 114, (Boundary-Layer Stability and Transition to Turbulence).

53. Saric, W.S., Hoos, J.A., Kohama, Y. and Radeztsky Jr., R.H. 1991 Boundary-Layer Receptivity to Sound with Roughness. Proc. ASME-FED Vol. 114, (Boundary-Layer Stability and Transition to Turbulence).

54. Saric, W.S. 1992 Laminar-Turbulent Transition: Fundamentals. Skin Friction Drag Reduction, AGARD Report 786, Ed. J. Cousteix.

55. Saric, W.S. 1992 The ASU Transition Research Facility. AIAA Paper No. 92-3910.

56. Lin, N., Reed, H.L. and Saric, W.S. 1992 Effect of Leading-Edge Geometry on Boundary-Layer Receptivity to Freestream Sound. ICASE Workshop on Stability and Transition. ed. M.Y. Hussaini, Springer-Verlag, New York.

57. Saric, W.S. 1994 Physical Description of Boundary-Layer Transition: Experimental Evidence. Progress in Transition Modelling, AGARD Report 793, Ed. W.S. Saric.

58. Saric, W.S. 1994 Görtler Vortices. Ann. Rev. Fluid Mech. Vol. 26, pp 379-409.

59. Benmalek, A. and Saric, W.S. 1994 Effects of Curvature Variations on the Nonlinear Evolution of Görtler Vortices. Phys. Fluids Vol. 6 (10), pp 3353-3367.

60. Saric, W.S., Reed, H.L. and Kerschen, E.J. 1994 Leading-Edge Receptivity to Sound. (Invited) AIAA Paper No. 94-2222.

61. Glauser, M., Chapman, K., Dagenhart, J. and Saric, W.S. 1994 Application of Multipoint Correlation Techniques to Aerodynamic Flows. (Invited) AIAA Paper No. 94-2278.

62. Radeztsky Jr., R.H., Reibert, M.S., and Saric, W.S. 1994 Development of Stationary Crossflow Vortices on a Swept Wing. AIAA Paper No. 94-2373.

63. Radeztsky Jr., R.H., Reibert, M.S., and Saric, W.S. 1995 Development of Stationary Crossflow Vortices on a Swept Wing. Laminar-Turbulent Transition. Vol. IV. pp 297-304. Ed. R. Kobayashi, Springer-Verlag, Berlin.

64. Saric, W.S., Wei, W. and Rasmussen, B.K. 1995 Effect of leading edge on sound receptivity. Laminar-Turbulent Transition. Vol. IV. pp 413-420. Ed. R. Kobayashi, Springer-Verlag, Berlin.


65. Kosorygin, V.V., Radeztsky Jr., R.H. and Saric, W.S. 1995 Laminar Boundary Layer Sound Receptivity and Control. Laminar-Turbulent Transition. Vol. IV. pp 417-524. Ed. R. Kobayashi, Springer-Verlag. ; also Preprint 92-19 I.T.A.M. Novosibirsk 1992 (in Russian).

66. Saric, W.S., Wei, W., Rasmussen, B.K. and Krutckoff, T.K. 1995 Experiments on Leading-Edge Receptivity to Sound. (Invited) AIAA Paper No. 95-2253.

67. Chapman, K.L., Glauser, M.N., Reibert, M.S. and Saric, W.S. 1995 Proper Orthogonal Decomposition Applied to Boundary-Layer Transition on a Swept Wing. Transitional Boundary Layers in Aeronautics, Royal Netherlands Academy of Arts and Sciences.

68. Reibert, M.S., Saric, W.S., Carrillo Jr., R.B., and Chapman, K.L. 1995 Nonlinear Stability, Saturation, and Transition in Swept-Wing Flows. (Invited) Transitional Boundary Layers in Aeronautics, Royal Netherlands Academy of Arts and Sciences.

69. Reibert, M.S., Saric, W.S. and Chapman, K.L. 1996 Experiments on Nonlinear Saturation of Stationary Crossflow Vortices in a Swept-Wing Boundary Layer. AIAA Paper No. 96-0184.

70. Chapman, K.L., Glauser, M.N., Reibert, M.S. and Saric, W.S. 1996 A Multi-Point Correlation Analysis of a Crossflow Dominated Boundary Layer. AIAA Paper No. 96-0186.

71. Reed, H.L., Saric, W.S. and Arnal, D. 1996 Linear Stability Theory Applied to Boundary Layers. Ann. Rev. Fluid Mech. Vol. 28, pp 389-428.

72. Reshotko, E., Saric, W.S. and Nagib, H. 1996 Turbulence and Noise Criteria and Their Implementation in NWTC-type wind tunnels. (Invited) AGARD CP-585, June 1997 pp. 28-1-14. Aerodynamics of Wind Tunnel Circuits and Their Components. Moscow

73. Reshotko, E., Saric, W.S. and Nagib, H. 1997 Flow Quality Issues for Large Wind Tunnels. (Invited) AIAA Paper No. 97-0255.

74. Reibert, R.S., Saric, W.S. 1997 Review of Swept-Wing Transition. (Invited) AIAA Paper No. 97-1816.

75. Reed, H.L., Haynes, T.S. and Saric, W.S. 1998 CFD Validation Questions in Transition Modeling. AIAA J. Vol. 36, No. 5, pp742-751.

76. Saric, W.S., Carrillo, R., Reibert, M. 1998 Leading-edge Roughness as a Transition Control Mechanism. AIAA Paper No. 98-0781.

77. Chapman, K., Reibert, M., Saric, W., Glauser, M. 1998 Boundary-Layer Transition Detection and Structure Identification through Surface Shear Stress Measurements. AIAA Paper No. 98-0782.

78. Saric, W.S. 1998 Control of Görtler Vortices. AGARD Report 827 High Speed Body Motion in Water, February 1998. pp. 8.1-5.

79. Saric, W.S., White, E. 1998 Influence of High-Amplitude Noise on Boundary-Layer Transition to Turbulence. AIAA Paper No. 98-2645.

80. Saric, W.S., Reshotko, E. 1998 Review of Flow Quality Issues in Wind Tunnels. (Invited) AIAA Paper No. 98-2613

81. Saric, W.S., Carrillo, R.B., Reibert, M.S. 1998 Nonlinear Stability and Transition in 3-D Boundary Layers. Meccanica Vol. 33: pp 469-87.

82. Saric, W.S., White, E.B., Reed, H.L. 1999 Boundary-Layer Receptivity to Freestream Disturbances and Its Role in Transition. (Invited) AIAA Paper No. 99-3788.

83. Radeztsky, R.H., Reibert, M.S., Saric, W.S. 1999 Effect of Isolated Micron-Sized Roughness on Transition in Swept-Wing Flows. AIAA J., Vol. 37, No. 11, pp. 1370-77.

84. White, E.B., Saric, W.S., Radeztsky, R.H. Jr. 2000 Leading-Edge Acoustic Receptivity Measurements Using a Pulsed-Sound Technique. Laminar-Turbulent Transition, Vol. V. Eds. W. Saric, H. Fasel, Springer-Verlag. . pp. 103-08. ISBN 3-540-679472.2


85. White, E.B., Saric, W.S. 2000 Application of Variable Leading-Edge Roughness for Transition Control on Swept Wings. AIAA Paper No. 2000-0283.

86. Reed, H., Saric, W.S. 2000 A Validation of the Parabolized Stability Equations for Three-Dimensional Boundary Layers (invited). ASME Paper No. FEDSM2000-11345.

87. Chen, K-P, Saric, W.S., Stone, H.A. 2000 On the Deviatoric Normal Stress on a Slip Surface. Physics of Fluids, Volume 12, No. 12, pp. 3280-1.

88. White, E.B., Saric, W.S., Gladden, R.D., Gabet, P.M. 2001 Stages of Swept-Wing Transition. AIAA Paper No. 2001-0271.

89. Monttinen, JT, Shortridge, RR, Latek, BS, Reed, HL, Saric, WS. 2001. Adaptive, Unstructured Meshes for Solving the Navier Stokes Equations for Low-Chord-Reynolds Number Flows. AIAA Progress in Astronautics and Aeronautics Vol. 195:60-80.

90. Reed, H.L., Saric, W.S., Lyttle, I., Asada, Y. 2001 Stability and Control of High-Speed Flows (Invited) AIAA Paper No. 2001-2700.

91. Saric, W.S., Reed, H.L. 2002 Supersonic Laminar Flow Control on Swept Wings Using Distributed Roughness. AIAA Paper No. 2002-0147.

92. Saric, W.S., Reed, H.L. 2002 Control of Transition in Supersonic Boundary Layers Using Distributed Roughness: Experiments and Computations. West East High Speed Flow Field (W.E.H.S.F.F.) Aerospace Applications from High Subsonic to Hypersonic Régime. ISBN 84-95999-18-8 pp. 417-25

93. Reed, H., Saric, W.S. 2002 CFD Validation Issues for Stability and Transition. (invited) ASME FED-SM2002-31366.

94. Saric, W.S., Reed, H.L. 2002 Control of Transition in Supersonic Boundary Layers: Experiments and Computations. (keynote paper) ASME FED-SM2002-31258.

95. Saric, W.S., Reed, H.L., Kerschen, E.J. 2002 Boundary-Layer Receptivity to Freestream Disturbances. Ann. Rev. Fluid Mech. Vol. 34, pp. 291-319.

96. Saric, W.S., Reed, H.L., White, E.B. 2003 Stability and Transition of Three-Dimensional Boundary Layers. Ann. Rev. Fluid Mech. Vol. 35, pp. 413-440.

97. Saric, W.S., Reed, H.L. 2003 Crossflow Instabilities: Theory and Technology (Invited). AIAA Paper No. 2003-0771.

98. White, E.B., Saric, W.S. 2005 Secondary Instabilities of Crossflow Vortices. J. Fluid Mech. Vol. 525:275-308.

99. Zuccher, S, Saric, W.S., Reed, H.L., McNeil, L.B. 2003 The Role of Infrared Thermography in the Study of Crossflow Instability at M = 2.4. Proceedings of the 7th International Symposium on Fluid Control, Measurement and Visualization, Sorrento, Italy 25-28 August 2003.

100. Monttinen, J, Reed, H.L., Squires, K.D., Saric, W.S. 2003 On the Effect of Winglets on the Performance of Micro-Aerial-Vehicles. Proceedings of the 1st ASU Symposium on Research in Engineering and Applied Sciences, Tempe, AZ. September 4, 2003.

101. Saric, W.S., Reed, H.L. 2004 Toward Practical Laminar Flow Control-Remaining Challenges (Invited). AIAA Paper No. 2004-2311.

102. Saric, W.S., Reed, H.L. 2005 Stability, Transition, and Control of Three-Dimensional Boundary Layers on Swept Wings. IUTAM: One Hundred Years of Boundary Layer Research Berlin: Springer, Ed: H. Heinemann.

103. Saric, W.S., Reed, H.L., Banks, D.W. 2005 Flight Testing of Laminar Flow Control in High-Speed Boundary Layers. RTO-MP-AVT-111/RSM.

104. Zuccher, S. Saric, W.S. 2006. Infrared Thermography Investigations in Transitional Supersonic Boundary Layers. Exps. Fluids. under review


Publications - EDITOR

1. "Stability in Convective Flows," Eds. W.S. Saric and A.A. Szewczyk, ASME Symposium Proceedings, HTD-Vol. 24, November 1985.

2. “Progress in Transition Modelling,” Ed. W.S. Saric, AGARD Report 793, March 1994.

3. “Reynolds Number and Mach Number Effects on Boundary Layer Structure,” Ed. W.S. Saric, AGARDograph AG-335, July 1996.

4. “Hypersonic Experimental and Computational Capability, Improvement, and Validation,” Eds: W S. Saric, J. Muylaert, C. Dujarric, AGARD Advisory Report 319, March, 1996.

5. “Laminar-Turbulent Transition, Volume V.” Eds. H. Fasel and W. Saric, Springer-Verlag, 2000. ISBN 3-540-67947-2.

Publications - Technical Reports

1. "A Generalized Magnetohydrodynamic Entrance-Flow Model - Part I: Momentum-Integral Method," W.S. Saric and K.J. Touryan, Sandia Corporation Research Report SC-RR-66-356, August 1966.

2. "A Generalized Magnetohydrodynamic Entrance-Flow Model - Part II: Series Solution," W.S. Saric and K.J. Touryan, SC-RR-66-357, September 1966.

3. "Problems of Hydrodynamic Stability Concerning Liquid-Gas Interfaces-Part I: Experimental Program," W.S. Saric, SC-TM-68-821, November 1968.

4. "Problems of Hydrodynamic Stability Concerning Liquid-Gas Interfaces-Part II: Analytical Program" W.S. Saric, SC-TM-68-870, February 1969.

5. "Body Force Effects on the Stability of a Liquid Film," A.H. Nayfeh and W.S. Saric, SC-RR-70-722, November 1970.

6. "The Rayleigh-Taylor Instability Applied to Liquid Drops," R.S. Bernard and W.S. Saric, SC-RR-70-725, September 1971.

7. "Nonlinear Motion of an Asymmetric Body with Variable Roll Rate," A.H. Nayfeh and W.S. Saric, SC-RR-72-0051, February 1972.

8. "Stability of Liquid Films Adjacent to Compressible Streams," G.L. Bordner, A.H. Nayfeh and W.S. Saric, Virginia Polytechnic Institute and State University Engineering Report, VPI-E-73-3, January 1973.

9. "Stability of Liquid Films on Transpiration-Cooled Reentry Vehicles, Part I: Supersonic Flows," W.S. Saric, A.H. Nayfeh and S.G. Lekoudis, VPI-E-75-21, October 1975.

10. "Stability of Liquid Films in Transpiration Cooling," W.S. Saric and K.J. Touryan, Sandia Technology, SAND 75-0426, 1975.

11. "Nonparallel Boundary-Layer Stability," W.S. Saric and A.H Nayfeh, Proceedings Second Low-Speed Boundary Layer Transition Workshop, RAND Corp., Santa Monica, California, September 1976, RAND/P-6119, January 1978.

12. "Design of a Three-Dimensional Traverse Mechanism for Boundary-Layer Stability Studies," W.T. Cousins, W.S. Saric and G.A. Reynolds, VPI-E-78-13, June 1978.

13 "Experiments on the Stability and Transition of Two-Dimensional and Three-Dimensional Boundary Layers with Suction," W.S. Saric and G.A. Reynolds, Final Report, NASA Grant NSG-1358, NASA-CR-157256, 1979.

14. "The Stability of Boundary Layers with Porous Suction Strips: Experiment and Theory," G.A. Reynolds, W.S. Saric, H.L. Reed and A.H. Nayfeh, Proceedings ACEE Project Oral Status Review, NASA-Dryden Flight Research Center, Edwards A.F.B., September 1981.


15. "Excitation of Wave Packets and Random Disturbances in a Boundary Layer," C. Costis and W.S. Saric, VPI-E-82.26, October 1982.

16. "Experiments on the Application of Suction Through Porous Strips for Laminar Flow Control," G.A. Reynolds and W.S. Saric, NASA Contractor's Report NASA-CR-161235, April 1983 (Also VPI-E-82.28).

17. "Computer Controlled Wind Tunnel Experiments: Part I. Peak-Valley Splitting of Unstable Waves," R.W. Henk and W.S. Saric, VPI-E-83.24.

18. "A Panel-Method Code to Design Wind-Tunnel Modifications for Pressure Gradients on Models: Part I. Inviscid Analysis," C.L. May and W.S. Saric, VPI-E-83.25.

19. "The Application of Nonlinear Stability Techniques to Boundary-Layer Transition," Th. Herbert and W.S. Saric, Final Report, Contract No. N60921-81-C-02844, NSWC, White Oak (1983).

20. "Boundary-Layer Transition: T-S Waves and Crossflow Mechanisms," W.S. Saric, Proc. AGARD Special Course on Aircraft Drag Prediction and Reduction, VKI, Belgium, AGARD Report No. 723, May 1985.

21. "Laminar Flow Control with Suction: Theory and Experiment," W.S. Saric, Proc. AGARD Special Course on Aircraft Drag Prediction and Reduction, VKI, Belgium, AGARD Report No. 723, May 1985.

22. "On The Three-Dimensional Structure of Boundary Layers Undergoing Transition to Turbulence," W.S. Saric, Final Report, AFOSR-82-0229, March 1985.

23. “Stability and Transition of Three-Dimensional Boundary Layers,” W.S. Saric and H.L. Reed, AGARD-CP-438, Fluid Dynamics of Three-Dimensional Turbulent Shear Flows and Transition

24 "The ASU Unsteady Wind Tunnel," W.S. Saric, ASU CEAS Tech. Rpt. CR-R 89030, April 1989.

25. "Boundary-Layer Receptivity, Part 1.: Freestream Sound and 2-D Roughness Strips," W.S. Saric, J.A. Hoos and Y. Kohama, ASU CEAS Tech, Rpt. CR-R-90091, May 1990.

26. "Experiments on Swept-Wing Transition (in Japanese)," S. Takagi and W.S. Saric, National Aerospace Laboratory Publication, SP-15, Sept. 1991.

27. “Crossflow Stability and Transition Experiments in Swept-Wing Flow”, J.R. Dagenhart and W.S. Saric, NASA Technical Publication, TP-1999-209344, pp. 1-132, July 1999.

Talks and Lectures by W.S. Saric

1. "A Generalized Magnetohydrodynamic Entrance Flow," (a) 5th U.S. National Congress of Applied Mechanics, University of Minnesota, Minneapolis, Minnesota, June 14-17, 1966; (b) Illinois Institute of Technology, Mechanics Seminar, Chicago, Illinois, April 1967.

2. "Sandia Liquid-Layer Stability Program," Reentry Vehicle Nosetip Symposium, Aerospace Corporation, San Bernardino, California, August 22, 1969.

3. "The Stability of Circular Couette Flow of Binary Mixtures," 6th U.S. National Congress of Applied Mechanics, Harvard University, Boston, Massachusetts, June 1970.

4. "An Experimental Investigation of the Stability of a Thin Liquid Layer Adjacent to a Supersonic Airstream," 3rd AIAA Fluid and Plasma Dynamics Conference, Los Angeles, California, June 1970, AIAA Paper No. 70-0801.

5. "Nonlinear Kelvin-Helmholtz Instability," 23rd Meeting of the Division of Fluid Dynamics, American Physical Society, Charlottesville, Virginia, November 23-25, 1970, Bull. Amer. Phys. Soc. 15, 1970.

6. "Experimental and Theoretical Investigations of the Stability of Liquid Films," (a) Workshop on Transpiration Cooling in Three-Dimensional Flow Fields, Aerospace Corporation, San Bernardino, California, January 5, 1971, (b) Virginia Polytechnic Institute and State University, Engineering Science and Mechanics Seminar, Blacksburg, Virginia, April 18, 1971.


7. "Nonlinear Motion of an Asymmetric Body with Variable Roll Rate," AIAA Guidance, Control, and Flight Mechanics Conference, Hofstra University, Hampstead, NEW YORK, August 16-18, 1971, AIAA Paper No. 71-0932.

8. "Stability of Liquid Films Interacting with Supersonic Streams: Theory and Experiment," (a) XII International Congress of Theoretical and Applied Mechanics, Moscow, U.S.S.R., August 21-26, 1972; (b) New York University, Guggenheim School of Aeronautics Seminar, New York, New York, December 12, 1972; (c) Illinois Institute of Technology, Mechanical and Aerospace Engineering Seminar, Chicago, Illinois, December 13, 1972.

9. "Nonlinear Stability of a Liquid Film Adjacent to a Supersonic Stream," 25th Mtg of the Div. of Fluid Dynamics, American Physical Society, Boulder, Colorado, Nov. 20-22, 1972, Bull. Amer. Phys. Soc. 17, 1972.

10. "Applications of Singular Perturbation Methods to Nonlinear Problems in Applied Mechanics," Reactor Analysis and Safety Division Seminar, Argonne National Laboratories, Argonne, Illinois, April 23, 1974.

11. "Nonparallel Boundary-Layer Stability," (a) Mechanical Engineering Seminar, Illinois Institute of Technology, Chicago, Illinois, April 22, 1974; (b) Mathematics Seminar, Rensselaer Polytechnic Institute, Troy, New York, April 29, 1974; (c) Mechanics Seminar, The Johns Hopkins University, Baltimore, Maryland, May 7, 1974; (d) Institute of Theoretical and Applied Mechanics, U.S.S.R Academy of Sciences, Novosibirsk, July 1, 1974; (e) Virginia Polytechnic Institute and State University, Blacksburg, Virginia, October 31, 1974; (f) University of Waterloo, Ontario, Canada, May 9, 1975; (g) Proceedings Second Low-Speed Boundary Layer Transition Workshop, RAND Corp., Santa Monica, California, September 13-15, 1976, RAND/P-6119, January 1978.

12. "Stability of Liquid Films Adjacent to Compressible Streams: Theory and Experiment," (a) Institute of Theoretical and Applied Mechanics, U.S.S.R., Academy of Sciences, Novosibirsk, July 1, 1974; (b) Colorado State University, Ft. Collins, Colorado, April 22, 1975; (c) 27th Annual Meeting Division of Fluid Dynamics, American Physical Society, Pasadena, California, November 25-27, 1974, Bull. Amer. Phys. Soc. 19, 1974.

13. "A Perturbation Method Applied to Two-Dimensional Hydrodynamic Stability Problems," Applied Mathematics Seminar, University of New Mexico, Albuquerque, New Mexico, April 29, 1975.

14. "Experiments on Supersonic Boundary-Layer Stability," (a) Virginia Polytechnic Institute and State University, Blacksburg, Virginia, June 19, 1975; (b) Institute of Theoretical and Applied Mechanics, U.S.S.R. Academy of Sciences, Novosibirsk, June 16, 1976.

15. "Rayleigh-Taylor Instability Applied to Pellet-Fusion Problems," Electron Beam Physics Group, Sandia National Laboratories, Albuquerque, New Mexico, October 27, 1975.

16. "Nonparallel Stability of Boundary-Layer Flows with Blowing or Suction," 28th Ann. Mtg. of the Div. of Fluid Dynamics, American Physical Society, Univ. Maryland, College Park, Maryland, November 25, 1975, Bull. Amer. Phys. Soc. 20, 1975.

17. "Perturbation Methods Applied to Problems of Nonlinear Mechanics," Institute of Theoretical and Applied Mechanics, U.S.S.R. Academy of Sciences, Novosibirsk, June 16, 1976.

18. "Experiments on Liquid-Film Stability," Ibid, Novosibirsk, U.S.S.R., June 24, 1976.

19. "Nonparallel Boundary-Layer Stability," Ibid, Novosibirsk, U.S.S.R., June 24, 1976.

20. "Stability of Stratified Flows," The Johns Hopkins University, Applied Physics Laboratories, Baltimore, Maryland, September 1976.

21. "Boundary-Layer Stability and Transition," Aerodynamics Group, Lockheed-Georgia Co., Marietta, Georgia, Jan. 13, 1977.

22. "Nonparallel Stability of Boundary-Layer Flows with Pressure Gradients and Suction," (a) Proceedings AGARD Symposium on Laminar-Turbulent Transition, Copenhagen, Denmark, May 2, 1977, AGARD CP. 224; (b) Institute a fur Mechanik, Universitat Stuttgart, F.R.G., May 13, 1977; (c) Institute fur Stromungslehre, Tech. Universitat Wein, Vienna, Austria, May 19, 1977.


23. "Experiments on Liquid-Film Stability," Lehrstuhl and Institute fur Thermishe Stromungsmachinen, Universitat Karlsruhe, F.R.G., May 10, 1977.

24. "Experiments on the Stability of Boundary Layers," 31st Annual Meeting of the Division of Fluid Dynamics, American Physical Society, Los Angeles, California, November 19-21, 1978, Bull. Amer. Phys. Soc. 23, 1978.

25. "Stability of 3-D Flows over Curved Walls," Proceedings XIV Biennial Fluid Dynamics Conference, Blaswziewko, Poland, September 1979.

26. "Experimental and Theoretical Investigations on Boundary-Layer Stability and Transition at VPI & SU," (a) Institute of Theoretical and Applied Mechanics, Novosibirsk, U.S.S.R., September 1979, (b) University of Tokyo, Japan, September 2, 1983.

27. "Experiments on the Stability of Nonlinear Waves in a Boundary Layer," I.U.T.A.M. Symposium on Laminar-Turbulent Transition, Stuttgart, F.R.G., September 1979, In: Laminar-Turbulent Transition, Springer, 1980.

28. "Nonlinear and 3-D Aspects of Boundary-Layer Transition," (a) The Johns Hopkins University, College of Engineering, Baltimore, Maryland, November 10, 1980; (b) Computing Seminar Series, Sandia National Laboratories, Albuquerque, New Mexico, January 15, 1981; (c) Howard University, Department of Mechanical Engineering, Washington, DC, April 3, 1981, (d) Lehigh University, Department of Mechanical Engineering, Bethlehem, Pennsylvania, July 11, 1981; (e) Institute of Theoretical and Applied Mechanics, Novosibirsk, U.S.S.R., August 27, 1981; (f) Proceedings XV Symposium on Advanced Problems and Methods in Fluid Mechanics, Jackranka, Poland, September 7, 1981.

29. "Visualization of Tollmien-Schlichting Waves," 33rd Annual Meeting of the Division of Fluid Dynamics, American Physical Society, Cornell University, Ithaca, New York, November 1980, Bull. Amer. Phys. Soc. 25, 1081.

30. "An Analysis of the Stability of Flows Over Concave Surfaces," Computing Seminar Series, Sandia National Laboratories, Albuquerque, New Mexico, January 16, 1981.

31. "Laminar Flow Control and Aircraft Energy Efficiency," (a) Solar Energy Research Institute, Golden, Colorado, January 19, 1981; (b) Florida State University, FAMU/FSU Institute for Engineering, Tallahassee, Florida, September 9, 1982.

32. "Resonant Three-Wave Interactions in Boundary Layers," (a) Institute of Mechanical Problems, Moscow, U.S.S.R., September 4, 1981; (b) University of St. Andrews, Mathematics Department, Scotland, U.K., September 15, 1981; (c) University of California - Los Angeles, Mechanics and Materials, Los Angeles, California, January 21, 1982; (d) The Johns Hopkins University, College of Engineering, Baltimore, Maryland, March 9, 1982; (e) Florida State University, FAMU/FSU Institute for Engineering, Tallahassee, Florida, September 9, 1982.

33. "The Stability of Boundary Layers with Porous Suction Strips: Experiment and Theory," (a) Institute of Theoretical and Applied Mechanics, Novosibirsk, U.S.S.R., August 26, 1981; (b) Institute of Mechanical Problems, Moscow, U.S.S.R., September 4, 1981; (c) Proceedings ACEE Project Oral Status Review, NASA-Dryden Flight Research Center, Edwards A.F.B., California, September 14-18, 1981.

34. "Predictions of Streakline Patterns of Unstable Waves in a Boundary Layer," Proceedings Symposium on Computers in Flow Prediction and Fluid Dynamics Experiments, ASME, WAM, November 1981.

35. "Computation and Visualization of Unstable-Wave Streaklines in a Boundary Layer," (a) 34th Annual Meeting of the Div. of Fluid Dynamics, American Physical Society, Naval Postgraduate School, Monterey, California, November 1981, Bull. Amer. Phys. Soc. 2, 1252; (b) University of Southern California, Applied Mechanics Seminar, Los Angeles, California, January 20, 1982.

36. "Boundary-Layer Stability and Transition Experiments with Blowing and Suction," (a) 35th Annual Meeting of the Division of Fluid Dynamics, American Physical Society, Rutgers University, New Brunswick, New Jersey, November 1982, Bull. Amer. Phys. Soc. 27, 1176, (b) AIAA 21st Aerospace Sciences Mtg, Reno, Nevada, January 1983, AIAA Paper No. 83-0043.


37. "Subharmonic Route to Turbulence in Boundary Layers," (a) Thermosciences Seminar, Stanford University, Palo Alto, California, January 13, 1983; (b) IUTAM Symposium on Turbulence and Chaotic Phenomena in Fluids, Kyoto, Japan, September 5-9, 1983; (c) Arizona State University, Tempe, Arizona, January 13, 1984; (d) University of New Mexico, Albuquerque, New Mexico, January 20, 1984; (e) University of California-San Diego, March 6, 1984; (f) University of Arizona, Tucson, Arizona, March 8, 1984; (g) DFVLR, Institut fur Theoretische Stromungsmechanik, Göttingen, West Germany, July 4, 1984, (h) GALCIT, Caltech, Pasadena, California, February 1985. (i) Princeton University, Princeton, New Jersey, February 11, 1986.

38. "An Orthogonal Coordinate Grid Following the 3-D Viscous Flow Over a Concave Surface," (a) Proceedings of Symposium on Grid Generation Methods, ASME Fluids Engineering Conference, June 20, 1983; (b) Sandia National Laboratories, Albuquerque, New Mexico, January 23, 1984.

39. "Forced and Unforced Subharmonic Resonance in Boundary-Layer Transition," (a) 36th Annual Meeting of the Division of Fluid Dynamics, American Physical Society, Houston, Texas, November 1983, Bull. Amer. Phys. Soc. 28, No. 9, 1983, (b) AIAA 22nd Aerospace Sciences Meeting, Reno, Nevada, January 1984, AIAA Paper No. 84-0007 ; (c) Illinois Institute of Technology, Chicago, Illinois, February 1, 1984.

40. "Design of High-Reynolds-Number Flat-Plate Experiments in the NTF," AIAA 9th Aerodynamic Testing Conference, San Diego, California, March 5-7, 1984, AIAA Paper No. 84-0588.

41. "Generation of Crossflow Vortices in a Three-Dimensional Flat-Plate Flow," (Invited) ASME Symposium on "Use of Artificial Excitation to Control Fluid Flows by Manipulating their Large-Scale Structure," ASME Applied Mechanics Conference, San Antonio, Texas, June 17-21, 1984; (b) Second IUTAM Symposium on "Laminar-Turbulent Transition," Novosibirsk, U.S.S.R., July 9-13, 1984; (c) 37th Annual Meeting of the Division of Fluid Dynamics, American Physical Society, Providence, Rhode Island, November 1984, Bull. Amer. Phys. Soc. 29.

42. "Experiments on the Stability of Crossflow Vortices in Swept-Wing Flows," (a) Inst. fur Theo. Stromungsmechanik, DFVLR, Göttingen, F.R.G., July 1984; (b) 23rd Aerospace Sciences Mtg., Reno, Nevada, January 1985, AIAA Paper No. 85-0493; (c) Aerospace Eng., University of Southern California, Los Angeles, California, April 1985; (d) Sandia National Laboratories, Albuquerque, New Mexico, June 12, 1985; (e) University of Houston, Houston, Texas, October 31, 1985.

43. "Stability and Transition in Bounded Shear Flows," (Invited) (a) Symposium on Perspectives in Fluid Mechanics, Caltech, Pasadena, California, January 1985, (b) Texas A&M University, College Station, Texas, November 1, 1985.

44. "The Görtler Instability," (Invited) AIAA Professional Study Series on Instabilities and Transition to Turbulence, Cincinnati, Ohio, July 13-14, 1985.

45. "Boundary-Layer Transition: T-S Waves and Crossflow Mechanisms," (Invited) (a) AGARD Special Course on Aircraft Drag Prediction and Reduction at VKI, Brussels, Belgium, May 20-24, 1985, (b) NASA Langley, Hampton, Virginia, August 19-21, 1985; AGARD Report No. 723.

46. "Laminar Flow Control with Suction: Theory and Experiment," (Invited) (a) AGARD Special Course on Aircraft Drag Prediction and Reduction at VKI, Brussels, Belgium, May 20-24, 1985, (b) NASA Langley, Hampton, Virginia, August 19-21, 1985, AGARD Report No. 723.

47. "Linear Stability: The Görtler and Other Nonparallel Problems," (Invited) International Workshop on Stability and Transition in Bounded Shear Flows, Tucson, Arizona, November 22-23, 1985.

48. "Oscillating Hot-Wire Measurements Above an FX63-137 Airfoil," (a) AIAA 24th Aerospace Sciences Mtg., Reno, Nevada, January 1986, AIAA Paper 86-0012; (b) 2nd Annual Arizona Fluid Mechanics Meeting, Tempe, Arizona, April 4-5, 1986.

49. "Initiating Chaos in Boundary Layers," (Invited) Chaotic Motion in Open Flows Workshop, UC Nonlinear Studies, Lake Arrowhead, California, February 7-9, 1986.

50. "Is Chaos Relevant to Shear Flows," Panelist: Chaotic Motion in Open Flows Workshop, UC Nonlinear Studies, Lake Arrowhead, California, February 7-9, 1986.


51. "ASU Unsteady Wind Tunnel," (a) AIAA 14th Aerodynamic Testing Conf. West Palm Beach, Florida, March 5-7, 1986, AIAA Paper No. 84-0588, (b) 2nd Annual Arizona Fluid Mechanics Meeting, Tempe, Arizona, April 4-5, 1986.

52. "Stability of Three-Dimensional Boundary Layers: Theory and Experiment," (Special Lecture) 3rd Asian Congress of Fluid Mechanics, Tokyo, Japan, September 1-5, 1986.

53. "Transition to Turbulence in Boundary Layers: The Last Five Years," (Invited Lecture) (a) 10th Symp. on Turbulence, Univ. Missouri, Columbia, Missouri, September 22-24, 1986; (b) NASA-Ames Research Center, Moffett Field, California, March 13, 1987; (c) University of Cincinnati, Cincinnati, Ohio, April 10, 1987, (d) ONERA, Toulouse France, May 18, 1987, (e) Institute de Mecanique des Fluids, Marseille France, May 21, 1987; (f) Univ. Minnesota, Twin Cities, Minnesota, February 2, 1988; (g) National Aerospace Laboratory, Tokyo, April 8, 1988, (h) Hokkaido Univ., Sapporo, Japan, April 13, 1988, (i) Univ. of Western Ontario, London, Canada, November 23, 1988.

54. "Experiments on Boundary-Layer Transition," (Invited), ICASE-NASA Langley Workshop on Stability and Transition, Hampton, Virginia, November 21, 1986.

55. "Stability of Hypersonic Attachment-Line Flows," (Invited), ICASE-NASA Langley Workshop on Stability and Transition of High Mach Number Shear Layers, Hampton, Virginia, March 20, 1987.

56. "Three-Dimensional Stability of Boundary Layers," (Invited), Symposium on Perspectives in Turbulence, Göttingen, F.R.G., May 11-15, 1987.

57. "Experiments on Unsteady Separation and Stall," ASME Applied Mechanics, Bioengineering and Fluids Engineering Conference, June 14-17, 1987.

58. "The ASU Unsteady Wind Tunnel and Fundamental Requirements for Freestream Turbulence Measurements" AIAA 26th Aerospace Sciences Meeting, Reno, Nevada, January 12-16, 1988, AIAA Paper No. 88-0053.

59. "On the Görtler Instability of Flows with Periodic Curvature," (Invited), (a) Symposium in honor of Itiro Tani, Tokyo, April 9, 1988; (b) Tohoku Univ., Sendai, Japan, April 11, 1988; (c) Fourth Arizona Fluid Mechanics Conference, Tucson, Arizona, April 30, 1988; (d) 41st Annual Meeting of the Division of Fluid Dynamics, American Physical Society, Buffalo, New York, November 1988, Bull. Amer. Phys. Soc. 33, 2283; (e) ICASE/NASA Langley Research Center Workshop on Instability and Transition, Hampton, Virginia, May 16, 1989.

60. "Stability and Transition in Three-Dimensional Boundary Layers," (Invited), AGARD Symposium on Fluid Dynamics of Three-Dimensional Turbulent Flows and Transition, Cesme, Turkey, October 3-6, 1988.

61. "Secondary Instabilities Leading to Transition," (Invited), E.R.C.O.F.T.A.C., Course on Physics of Transition from Laminar to Turbulent Flow, Politecnico di Torino, Torino, Italy, October 13, 1988.

62. "Three-Dimensional Transition," (Invited), E.R.C.O.F.T.A.C., Course on Physics of Transition from Laminar to Turbulent Flow, Politecnico di Torino, Torino, Italy, October 14, 1988.

63. "Experiments in Swept-Wing Transition," (Invited), Fourth Symposium on Numerical and Physical Aspects of Aerodynamic Flows, Long Beach, California, January 16-19, 1989.

64. "Control of Random Disturbances in a Boundary Layer," (a) 2nd AIAA Shear Flow Control Conference, March 13-16, 1989, AIAA Paper No. 89-1007; (b) Fifth Arizona Fluid Mechanics Conference, Tucson, Arizona February 1989.

65. "Experiments in 3-D Boundary-Layer Stability and Transition," (a) University of Southern California, Los Angeles, California, April 5, 1989; (b) University of California-Berkeley, April 6, 1989; (c) Third I.U.T.A.M. Symposium on Laminar-Turbulent Transition, Toulouse, France, September 11-15, 1989; (d) Hiroshima University, Japan, September 20, 1989; (e) University of Osaka Prefecture, Japan, September 22, 1989, (f) University of Tokyo, October 3, 1989; (g) 42nd Annual Meeting of the Division of Fluid Dynamics of the American Physical Society, November 19-21, 1989, Bull. Amer. Phys. Soc. 34, p. 2249.


66. "Sources of Error in Low-Speed Stability Experiments," (Invited), ICASE/NASA Langley Research Center Workshop on Instability and Transition, Hampton, Virginia, June 1, 1989.

67. "Boundary-Layer Stability and Transition," (Invited Keynote Lecture), Fifth International Conference on Numerical Ship Hydrodynamics, Hiroshima, Japan, September 25-28, 1989.

68. "Boundary-Layer Receptivity to Freestream Turbulence and Sound," 42nd Annual Meeting of the Division of Fluid Dynamics of the American Physical Society, November 19-21, 1989, Bull. Amer. Phys. Soc. 34, p. 2260.

69. "Boundary-Layer Receptivity: Experiments," (Invited), Third International Congress of Fluid Mechanics, Cairo, Egypt, January 2-4, 1990.

70. "Boundary-Layer Receptivity, Part 1.: Freestream Sound and 2-D Roughness Strips," 13th National Congress of Applied Mechanics, Univ. Arizona, Tucson, Arizona, May 21-25, 1990.

71. "A High-Frequency, Secondary Instability of Crossflow Vortices That Leads to Transition," (a) Görtler Vortex Flows, EUROMECH 261, June 13, 1990, Nantes, France, (b) NASA-Langley Research Center, Hampton Virginia, August 15, 1990.

72. "Summary of Görtler Vortex Research -- Euromech 261 and The Future," (Invited), Görtler Vortex Flows, EUROMECH 261, June 14, 1990, Nantes, France.

73. "Visualization of Low-Reynolds-Number Flow Fields Around Receptivity Elements," 43rd Annual Meeting of the American Physical Society, November 18-20, 1990, Bull. Amer. Phys. Soc. Vol. 35, p. 2262.

74. "Boundary Layer Transition Control Using Receptivity," AFOSR Mtg on Turbulence Structure and Control, April 1-3, 1991.

75. "Surfaces Nonuniformity Effects on Stability and Transition," (a) NASA-Langley Research Center, Hampton, Virginia, April 24. 1991, (b) NASA-Ames Research Center, Moffett Field, California, May 16, 1991, (c) 44th Annual Meeting of the American Physical Society, November 24-26, 1991, Bull. Amer. Phys. Soc. Vol. 36, 2630.

76. "Görtler Vortices With Periodic Curvature," Proc. Boundary-Layer Stability and Transition to Turbulence, ASME/FED, June 17, 1991.

77. "Boundary Layer Receptivity to Sound with Roughness," Proc. Boundary-Layer Stability and Transition to Turbulence, ASME/FED, June 18, 1991.

78. "Thither Transition To Turbulence," (Invited Plenary Lecture), (a) ASME Applied Mechanics Division Summer Meeting, June 12, 1991; (b) Symposium in Honor of Eli Reshotko, NASA-Langley/ICASE, Hampton, Virginia, July 28, 1991.

79. "Applications of Laminar-Turbulent Transition: High Speed Transports," Special Lecture Notes No. 359, Aeronautics and Astronautics, Tohoku University, Sendai, Japan, November 7, 1991.

80. "Role of Micron-sized Roughness in Transition of Swept-wing Flows," (a) NASA-Ames Research Center, Moffett Field, California, February 27, 1992; (b) Eighth Annual Arizona Fluid Mechanics Conference, February 28, 1992; (c) Institute of Fluid Sciences, Sendai Japan, Mar 24, 1992 (d) NASA-Langley Research Center, Hampton, Virginia, July 30, 1992 (e) (Invited) Institut de Mécanique Statistique de la Turbulence, Marseille, France, May 28, 1993.

81. "Laminar-Turbulent Transition: Fundamentals," Special Course on Skin Friction Drag Reduction, AGARD Report 786, Brussels, Belgium, March 1992.

82. "The ASU Transition Research Facility." (Invited) AIAA 17th Aerospace Ground Testing Conference, Nashville, Tennessee, July 6, 1992, AIAA Paper No. 92-3910.

83. "Nonlinear Development of Görtler Vortices over Variable Curvature Surfaces." (a) NASA-Langley Research Center, Hampton, Virginia, July 30, 1992, (b) International Taylor-Couette Symposium, Nice, France, March 30, 1993.


84. "Boundary-Layer Receptivity: Freestream Sound on an Elliptical Leading Edge." 45th Annual Meeting of the American Physical Society, November 22-24, 1992, Bull. Amer. Phys. Soc. Vol. 37, 1720.

85. "Boundary-Layer Transition: Experimental Evidence," Special Course on Progress in Transition Modelling, AGARD Report 794, (a) Madrid, Spain, March 22, 1993, (b) Brussels, Belgium, March 29, 1993.

86. "Low-Speed Boundary-Layer Transition," ICASE/NASA Short Course on Experimental Methods Related to Instabilities and Transition to Turbulence, Hampton, Virginia, June 2, 1993.

87. "Receptivity: Initial-Value Problems for Transition to Turbulence," (Invited G.I. Taylor Lecture), ASCE/ASME/SES Summer Meet'n '93, Univ. Virginia, Charlottesville, Virginia, June 8, 1993.

88. "Nonlinear Stability and Transition in 3-D Boundary Layers," (a) University of Arizona, Tucson, Arizona October 1993; (b) (Invited) Hypersonics Workshop, NASA-Langley Research Center, Hampton, Virginia, November 1, 1993; (c) (Invited) Symposium on Innovations in multiphase flow. University of Minnesota, Twin Cities, Minnesota March 26, 1994; (d) (Invited) CERT-ONERA, Toulouse France, June 8, 1994; (e) (Invited) 2nd International Conference on Experimental Fluid Mechanics, Torino, Italy, July 6, 1994.

89. “Leading-Edge Receptivity to Sound,” (a) (Invited) CERT-ONERA. Toulouse France, June 8, 1994; (b) (Invited) AIAA 25th Fluid Dynamics Conference, Colorado Springs, Colorado, June 20, 1994. AIAA Paper No. 94-2222.; (c) 4th IUTAM Symposium on Laminar-Turbulent Transition, Sendai, Japan, September 4, 1994; (d) (Invited) DLR, Göttingen, Germany, October 20, 1994; (e) (Invited) Universität Stuttgart, Stuttgart, Germany, October 21, 1994; (f) 47th Annual Meeting of the American Physical Society, November 20-22, 1994, Bull. Amer. Phys. Soc. Vol. 39.

90. “Development of Stationary Crossflow Vortices on a Swept Wing,” (a) 4th IUTAM Symposium on Laminar-Turbulent Transition, Sendai, Japan, September 4, 1994; (b) (Invited) GALCIT, Caltech, Pasadena, CA, October 28, 1994.

91. “Experiments on Leading-Edge Receptivity to Sound,” (a) (Invited) AIAA 26th Fluid Dynamics Conference, San Diego, California, June 21, 1995, AIAA Paper No. 95-2253; (b) Illinois Institute of Technology, Chicago, Illinois, January 31, 1996; (c) (Invited) Royal Technical Institute, Stockholm Sweden, March 29, 1996; (d) (Invited) IATF-Kernforschungszentrum, Karlsruhe, Germany, September, 24, 1996; (e) (Invited) Max Planck Institute, Göttingen, Germany, September, 26, 1996.

92. "Nonlinear Stability, Saturation, and Transition in Swept-Wing Boundary Layers," (a) (Invited) Colloquium on Transitional Boundary Layers in Aeronautics, Royal Netherlands Academy of Arts and Sciences, Amsterdam, December 6, 1995; (b) (Invited) Stanford University, Palo Alto, California, January 23, 1996; (c) (Invited) Purdue University, West Lafayette, Indiana, February 1, 1996; (d) Northwestern University, Evanson, Illinois, February 2, 1996; (e) (Invited) Beer Sheva Seminar on MHD and Turbulence, Jerusalem, Israel, February 26, 1996.

93. "Localized Roughness Effects on Transition in Three-Dimensional Boundary Layers," (a) (Invited) Israel Aircraft Industries, Tel Aviv, Israel, February 28, 1996; (b) (Invited) EUROMECH Colloquium 335 on Dynamics of Localized Disturbances, Karlsruhe, Germany, April 1, 1996.

94. “Puzzles in Transition of Hypersonic Boundary Layers,” NATO Workshop on Hypersonic Flows, Paris, France, April 11-12, 1997.

95. "Influence of High-Amplitude Noise on Boundary-Layer Transition to Turbulence," (a) AFOSR Workshop on Turbulence and Control, Hampton Virginia, August 13-15, 1997; (b) Syracuse University Workshop on Transition in Turbines, Minnowbrook, New York, September 8-10, 1997.

96. “Distributed Roughness Effects on Swept-Wing Transition,” (a) (Invited) Notre Dame University, South Bend, Indiana, November 1, 1996; (b) NASA-Langley Research Center, Hampton, Virginia, November 15, 1996.

97. “Control of Görtler Vortices,” [Invited] NATO Workshop on High Speed Body Motion in Water, Kiev Ukraine, September 1-3, 1997.


98. “Nonlinear Stability and Saturation in 3-D Boundary Layers,” [Invited] 50th Annual Meeting of the American Physical Society, Division of Fluid Dynamics, November 23-25, 1997, Bull. Amer. Phys. Soc. Vol. 42, No. 11, p 2260.

99. “Leading-Edge Roughness as a Transition Control Mechanism,” (a) AIAA 36th Aerospace Sciences Meeting, Reno, Nevada,. January 15, 1998, AIAA Paper No. 98-0781; (b) Northrop Grumman, , Pico Rivera, California January 16, 1998; (c) International Conference in Memory of Professor Carlo Ferrari, Torino, Italy, April 3, 1998; (d) IUTAM Symposium on Flow Control, Göttingen, Germany, September 8, 1998; (e) Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing, China November 3, 1998; (f) Department of Mechanics, Peking University, Beijing, China, November 6, 1998.

100. “Review of Flow Quality Issues in Wind Tunnel Testing (Invited) AIAA 20th Advanced Measurement and Ground Testing Technology Conference, Albuquerque, New Mexico, June 15-18, 1998, AIAA Paper No. 98-2613.

101. “Influence of High-Amplitude Noise on Boundary-Layer Transition to Turbulence” (a) AIAA 20th Advanced Measurement and Ground Testing Technology Conference, Albuquerque, New Mexico, June 15-18, 1998, AIAA Paper No. 98-2645; (b) Euromech Symposium on Laminar-Turbulent Transition, Göttingen, Germany, Sept. 14, 1998; (c) Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing, China November 2, 1998; (d) Department of Mechanics, Peking University, Beijing, China, November 6, 1998;. (e) GALCIT, Caltech, Pasadena, California, November 13, 1998; (f) 51th Annual Meeting of the American Physical Society, Division of Fluid Dynamics, November 22-24, 1998, Bull. Amer. Phys. Soc. Vol. 43, No. 11; (g) 13th Australian Fluids Mechanics Conference, Monash University, Australia, December 16, 1998.

102. “Stability and Transition in 3-D Boundary Layers” (Invited) University of California Los Angeles (UCLA) Los Angeles, California, February 12, 1999.

103. “Control Transition in 3-D Boundary Layers” (Invited) Brown University, Providence, Rhode Island, March 23, 1999.

104. “The use of MEMS to Control Transition in 3-D Boundary Layers” (Invited) Case Western Reserve University, Cleveland, Ohio, March 24, 1999.

105. “The Role of Stability in Transition to Turbulence” (Invited) The National Center for Microgravity Research, 98-99 Fluids Lecture Series (9 hour invited guest lecture) NASA Lewis Research Center, Cleveland, Ohio, March 25-26, 1999.

106. “The Need for Remote Real-time Measurements of MEMS Actuators in a Transition-Control Experiment” (Invited) VibraScan User’s Meeting, Polytech PI Incorporated, June 8, 1999.

107. “Validation of an Acoustic-Receptivity Experiment Using a PSV” (Invited) VibraScan User’s Meeting, Polytech PI Incorporated, June 8, 1999.

108. “Boundary-Layer Receptivity to Freestream Disturbances and Its Role in Transition” (Invited) 30th AIAA Fluid Dynamics Conference, Norfolk, VA. July 1, 1999 AIAA Paper No. 99-3788.

109. “Control of Transition in Swept-Wing Boundary Layers Using MEMS Devices as Distributed Roughness” (Invited) Defense Advanced Research Projects Agency (DARPA) DoD-Wide MEMS Meeting, Salt Lake City, Utah, July 7, 1999.

110. “Stability and Transition in 3-D Boundary Layers” (invited lecture), C.I.R.A. (Centro Italiano Ricerche Aerospaziali) 3rd ERCOFTAC SIG 33 Workshop, New and Emerging Techniques for Transition Prediction, Ravello, Italy, April 27-28, 2000

111. “A Validation of the Parabolized Stability Equations for Three-Dimensional Boundary Layers” (invited paper), 2000 ASME Fluids Engineering Summer Conference, Boston, MA. June 11-15, 2000. ASME Paper No. FEDSM2000-11345.


112. “Transition on Swept Wings” (a) (invited keynote lecture), ICAS 2000 Congress, Harrogate, United Kingdom, August 25-September 1, 2000, (b) Dept. Aerospace Engineering, Texas A&M Univ. February 21 2001 (c) Cornell University Ithaca, NY. June 25, 2001 (d) Swiss Federal Institute of Technology, Zurich, Switzerland, January 8, 2002 (e) Ecole Polytechnique Federale de Lausanne, Lausanne, Switzerland, January 9, 2002.

113. “Control of Transition in 3-D Boundary Layers with Streamwise Vortices in the Presence of Freestream Turbulence and Random Surface Roughness” (a) International Workshop on Organized Vortical Motion as a Basis for Boundary-Layer Control” Kiev, Ukraine, September 20-22, 2000 (b) ONERA-CERT Toulouse France, October 16, 2000 (c) 53rd Annual Meeting of the American Physical Society, Division of Fluid Dynamics, November 19-21, 2000, Bull. Amer. Phys. Soc. Vol. 45, No. 11 (d) Boeing, Long Beach, CA. February 7, 2001 (e) Lockheed Skunkworks, Palmdale, CA. February 14, 2001 (f) Northrop-Grumman, El Segundo, CA. May 25, 2001 (g) Boeing Military Systems, Seattle, WA. August 15, 2001.

114. “Measurement of Laminar-Turbulent Transition Behavior” Workshop on Prediction of Laminar-turbulent Transition in Boundary Layers, Tokyo, Japan, September 27-29, 2000.

115. “Receptivity Effects in Transition Control” W.S. Saric, 53rd Annual Meeting of the American Physical Society, Division of Fluid Dynamics November 19-20, 2000, Bull. Am. Phys. Soc. Vol. 45, No. 11.

116. “Boundary-Layer Receptivity to Freestream Sound” EuroMech Colloquim 423, 2-4 April 2001, Stuttgart, Germany.

117. “Supersonic Laminar Flow Control on Swept Wings Using Distributed Roughness” (a) 54th Annual Meeting of the American Physical Society, Division of Fluid Dynamics San Diego, CA. November 18-20, 2001 (b) 40th Aerospace Sciences Meeting & Exhibit, Reno, Nevada, January 14-17 2002 AIAA Paper No. 2002-0147 (c) Lockheed Martin Aerospace, Ft. Worth, TX. August 15, 2002, (d) GE Aircraft Engines, Cincinnati, OH August 21, 2002.

118. “Control of Transition in Supersonic Boundary Layers: Experiments and Computations”(keynote paper) 2002 ASME Joint U.S.-European Fluids Engineering Division Summer Meeting, Montreal, Quebec, Canada, July 14-18, 2002 ASME FED-SM2002-31258.

119. “High-Frequency/Low-Frequency Flow Control Applied to Swept-Wing Transition” (Invited) 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 6-9, 2003 AIAA Paper No. 2003-0536.

120. “Crossflow Instabilities: Theory and Technology” (Invited) 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 6-9, 2003, AIAA Paper No. 2003-0771.


7 MAJOR PROJECTS AT TEXAS A&M UNIVERSITY

Three major projects are being completed by W.S. Saric at Texas A&M University. The facilities and flight laboratory are for both undergraduate and graduate use.

Klebanoff/Saric Unsteady Wind Tunnel

The Klebanoff/Saric Unsteady Wind Tunnel is a major research facility that was moved to A&M from Arizona State University in 2004. This is an internationally recognized low-turbulence wind tunnel within which the most sensitive boundary-layer stability experiments can be conducted. It is only one of five low-speed wind tunnels in the world that have this capability (A&M, IIT-Chicago, Novosibirsk, Sendai, Stockholm). The length, width, and height of the tunnel are 86x25x20 ft respectively. The test section is 16x4.5x4.5 ft. A new 3,000 sq ft building is designed and will be submitted for approval. Tunnel assembly will commence under the direction of Drs. Saric and Bowersox after the building is completed. Construction and assembly costs are financed through a $400,000 grant from AFOSR, $25,000 each from the Boeing Company and Bell Helicopter, and funds from the Oran Nicks Wind Tunnel, the Aerospace Engineering Department, and research overhead. Operations are expected to resume in early 2007. When completed, its estimated worth will be $2,500,000. See http://flight.tamu.edu for progress reports and completion dates.

NASA-Langley Mach 6 Quiet Tunnel

The NASA-Langley Mach 6 Quiet Tunnel was de-commissioned at NASA-LaRC and was moved to A&M by Profs. Reed, Saric, and Bowersox in 2005 with the support and encouragement of AFOSR. This is a very special, internationally recognized tunnel where the noise levels are reduced to a level that permits the conduct of sensitive boundary-layer stability experiments. It is one of only three tunnels world-wide that have this capability in the supersonic flight regime (A&M, Purdue, NASA-LaRC Mach 3.5). It is presently being re-assembled under the direction of Drs. Bowersox and Saric in the North part of the Oran Nicks Wind Tunnel building and will be part of the National Aerothermochemistry Laboratory. Construction and assembly costs are financed through a $300,000 grant from AFOSR, and funds from the Aerospace Engineering Department. Operations are expected to begin in fall 2006. When completed its estimated worth will be over $3,000,000. See http://flight.tamu.edu for progress reports and completion dates.

Flight Research Laboratory

The aircraft, laboratories, offices, students, and staff of the Flight Research Laboratory are located in hanger 1091 at the General Aviation facilities at Easterwood Airport across the street is the Wind Tunnel Complex housing the 7x10 Oran Nicks Wind Tunnel, the National Aerothermochemistry Laboratory, and the Klebanoff/Saric Unsteady Wind Tunnel.

The laboratory has three aircraft: the Cessna O-2 (military version of the Cessna 337 Skymaster) for heavy instrumentation, observation, and data transmission; the Stemme S-10 VT powered sailplane for its ultra-low disturbance environment, and high-altitude capabilities; and the Velocity XL-5 for its high-speed, pusher configuration. Experiments are conducted on specially designed models or extensions that do not compromise the flight characteristics of these aircraft. Research concentrates on boundary-layer stability and transition, air-quality measurements over major Texas cities, and sensor and instrumentation development for flight applications. See http://flight.tamu.edu for progress reports.


8 ASU WIND TUNNEL PROJECTS

Three major wind-tunnel projects were completed by W.S. Saric at ASU. The facilities are for both undergraduate and graduate use and are of sufficiently good flow quality to be used for research projects.

Unsteady Wind Tunnel Project

The ASU Unsteady Wind Tunnel is a major research facility that was established at ASU by W. S. Saric. This effort involved the acquisition and transport of key elements from the Klebanoff tunnel at the National Bureau of Standards, building construction at ASU, redesign and construction of 75% of the tunnel, purchase of supplies, tools, and instrumentation, and the accounting and subcontracting as well as the supervision of staff and student workers. The building was completed June 1985 and the tunnel became operational December 1987 with total expenditures of over $1,000,000 from University, Federal Agency, and Local Industry support. Present worth $2,500,000.

0.2 meter Supersonic Wind Tunnel Project

The ASU 0.2 m Supersonic Tunnel was a pilot tunnel at NASA-Ames that was moved to ASU. It has been completely reconditioned and modernized by W.S. Saric. The tunnel has a 0.2 m x 0.18 m cross-section with Mach 2.4, 3.0, and 3.5 nozzles. It is blowdown to atmosphere with a maximum reservoir pressure of 35 atm. Computer-controlled valves to regulate stagnation pressure have been added, along with four new compressors, dryers, a sub-micron filter system, flow-uniformity screens, a 3-D traverse, a new schlieren system, Infra-Red Thermography, and a variable Mach number, variable pressure, hotwire calibration tunnel. This represents an additional investment by ASU and Federal Agencies of $500,000.

Flow Visualization Wind Tunnel Project

The ASU Flow Visualization Tunnel is a facility that was designed and built by W.S. Saric and the Unsteady Wind Tunnel staff. The dual-use design of the tunnel permits it to be used in undergraduate laboratory instruction as well as in low-cost research operations where preliminary and diagnostic experiments can be carried out. This facility is a low-turbulence, in-draft tunnel with a 0.5 m octagonal (0.54 m diagonal) test section that is 2.4 m long. Honeycomb and screens reduce the disturbance levels to 0.1%. A contraction ratio of 25:1 facilitates creating laminar smoke filaments for visualization. See: http://wtsun.eas.asu.edu for details.

9 SPONSORED RESEARCH ACTIVITIES

Texas A&M University

Since 1 Jan 05, responsible for $1,795,626 of active contracts.

ACTIVE AND RECENT CONTRACTS

“Flight experiments on laminarization of swept-wing boundary layers using periodically distributed roughness elements,” Universal Technology Corp (Prime sponsor Air Force Research Laboratory - AFRL), PI: William Saric, 3 graduate students, 1/Jun/05 – 19/May/06, $341,388. 100% Saric, 100% external.

“Flight experiments on local and global effects of surface roughness on 2-D and 3-D boundary-layer stability and transition,” AFOSR/NA, PI: William Saric, 3 graduate students, 1/Jan/05 – 30/Sep/07, $905,070. 100% Saric, 100% external.

“Acquisition and installation of the Saric/Klebanoff Low-Turbulence Unsteady Wind Tunnel,” DURIP/AFOSR, PI: William Saric, 1 graduate student, 1 May 05 – 30 April 06, $93,692. 100% Saric, 100% external.


“MURI (04) Hypersonic Transition and Turbulence etc.,” AFOSR, PI. S. Girimaji, ½ graduate student, 1 May 05 – 30 April 06, $305,560 added to existing MURI for installation of the Saric/Klebanoff Wind Tunnel. 100% Saric, 100% external.

“Swept-wing laminar flow wind-tunnel test” Northrop-Grumman Corporation, PI: William Saric, 3 graduate students, 15 Jun 05 – 30 Sep 05, $33,546. 100% Saric, 100% external.

“Airborne Sampling in Texas of Ozone and Precursors,” Univ. Texas – Austin, PI: William Saric (82%), Co-PI: Don Collins (18%),15 Aug 05 – 31 Aug 06, $88,519. (a three-part contract that is continuing).

“REMS Flight Test,” General Electric, PI: William Saric (100%), 1 Dec 05 – 31 Dec 05, $27,851, 100% external.

Arizona State University

Principal investigator on external research and equipment projects with sponsor totals of $9.0 million. Levels of responsibility on these projects total $8.0 million during 20 years. “Flight Experiments on Laminarization of Swept-Wing Boundary Layers Using Periodically Distributed Roughness Elements” Universal Technology Corporation, 22/Jun/04 —30/Apr/05, $377,944.

“Flow Quality Measurements in the NASA-Ames 11 ft Unitary Plan Tunnel (UPT)” Northrop Grumman Corporation, 1/Dec/04 — 31/Dec/04, $6,213.

“Spatial and Temporal Resonances in Hydrodynamics: A Theoretical, Experimental, and Numerical Exploration,” National Science Foundation, 01/Apr/00-31/Mar/03 Juan Lopez, PI, W. Saric, Co-PI, $244,125, responsible for$122,062.

“Supersonic Laminar Flow Control on Swept Wings Using Distributed Roughness,” DARPA. 1/Dec/00 – 30/Mar/03, Helen Reed Co-PI, $1,132,318, responsible for $733,522.

“Supersonic Laminar Flow Control on Swept Wings- Extension,” DARPA. 1/Apr/00 – 31/Dec/05, Helen Reed Co-PI, $1,195,000 responsible for $700,000.

“Design and Stability Characteristics of a QSP Airfoil,” Lockheed-Martin Skunkworks. 1/Jun/01 – 31/Dec/02. Helen Reed Co-PI, $168,910, responsible for $59,118.50

“Pulsed-Sound Measurements of the Influence of High-Amplitude Noise on Boundary-Layer Transition to Turbulence,” Air Force Office of Scientific Research, 15/Nov/99-14/Nov/02, $224,364.

“High Lift Over Drag Active (HiLDA) Wing,” Lockheed Martin Aeronautics. 21/Jan/02-20/Dec/02 $43,209, responsible for $15,123.15.

“Boundary-Layer Receptivity measurements Using Acoustic Wave-Packet Forcing,” National Science Foundation, 01/Oct/99-30/Sep/02, $227,903.

“Control of Transition in Swept-Wing Boundary Layers Using MEMS Devices as Distributed Roughness,” Air Force Office of Scientific Research, 1/Jul/97-31/Dec/00, Helen Reed, Co-PI, responsible for $884,969.

“National Defense Science & Engineering Graduate Fellowship Program,” Department of Defense, 1/Aug/98-31/Aug/00, $40,844.

“Aerodynamic Studies of Micro Air Vehicles,” Air Force Office of Scientific Research, 01/Sep/98-30/Sep/01, Helen Reed, PI, W. Saric, Co-PI, $334,244, responsible for $167,122


“University Micro Aerial Vehicle Competition,” Sanders, A Lockheed-Martin Company, 26/Jan/99-31/May/00, Helen Reed, W. Saric, Co-Principal Investigators, $9,000.

“IUTAM Symposium: Laminar-Turbulent Transition,” National Science Foundation, 15/Sep/99-31/Aug/00, $9,775.

“IUTAM Symposium: Laminar-Turbulent Transition,” Office of Naval Research, 01/Aug/99-31/Dec/99, $10,000.

“Leading-Edge Roughness as a Transitional Control Mechanism”, Northrop Grumman Corporation, 16/Oct/98-15/Apr/99, $31,540.

"Influence of High-Amplitude Noise on Boundary-Layer Transition to Turbulence," Air Force Office of Scientific Research, 15/Jul/96-15/Jul/98, $319,734.

“Scanning Laser Vibrometer for MEMS Control Devices,” Air Force Office of Scientific Research, 03/Mar/98 - 01/Jul/98, $146,375.

“Swept-Wing Receptivity Studies with Roughness,” NASA-Langley Research Center, Cooperative Agreement NAG 1 1925, 1/Jun/97-31/Oct/98, $144,184.

“Active Flow Control on Hurley’s Free-Streamline Airfoil and Delta Wing,” Air Force Office of Scientific Research, 1/Mar/98 - 31/Aug/98, I. Wygnanski (UA) Principal Investigator; E. Madenci (UA), W. Saric, H. Reed, Co-Principal Investigators, $100,000.

"Effects of Suction on Swept-Wing Transition," NASA Langley Research Center, Cooperative Agreement NAC-1-194, 1/Jun/94 - 15/Dec/97, $269,938.

"Receptivity and Control of Boundary Layers Influenced by Body Forces," National Research Council. 18/Jan/96-31/Dec/97, $13,060.

"Dynamic Calibration of Hot-Film Sensors Using Controlled Instability Waves," Clarkson University, 375-566-1, 1/Aug/95-31/Jul/97, $59,985.

"Effects of Suction on Swept-Wing Transition," Boeing Commercial Airplane Group, 1/Apr/96-31/Dec/96, $49,849.

"Surge Control Valve Test," Scientific Monitoring, Inc., 5/Apr/96-30/Sep/96, $6,980.

"Control of Unstable Waves in Three-Dimensional Boundary Layers," NASA Langley Research Center, Fellowship GR-NAG1-1111, 23/Feb/90 - 31/Aug/95, $255,202.

"Receptivity in Boundary-Layer Transition to Turbulence," Air Force Office of Scientific Research, F49620-94-002-1, 15/Oct/93 - 30/Sep/95, $204,999.

“Application of multi-point correlations techniques to a 3-D transitional flow,” Clarkson University, 1/Aug/94-31/Jul/95, $34,972

“Aerodynamics of the Large-Flow-Through Detector,” Los Alamos National Laboratory, 1/Jun/94-31/Dec/94, Co-PI with H.L. Reed and D.L. Laananen, $33,832, responsible for $11,000.

"Flat Plate Experiments in the National Transonic Facility," NASA Langley Research Center, 22/Oct/84 - 30/Dec/87, $101,137.


"Three-Dimensional Structure of Transitional Boundary Layers," Air Force Office of Scientific Research, 5/Jun/85 - 14/Nov/89, $393,654.

"Boundary-Layer Stability in Laminar Flow Control," NASA Langley Research Center Grants NAG 1-598, NAG 1-805, and NAG 1-1032, 15/Jun/85 - 31/Dec/89, $180,278.

"Unsteady Low-Reynolds-Number Aerodynamics," Office of Naval Research, 16/Jun/85 - 30/Sep/89, $217,600.

"Multi-Axis, 3-D, Scanning LDA System for Unsteady Aerodynamics," Air Force Office of Scientific Research, 1/Oct/86 - 30/Sep/88, $148,974.

"Stability and Transition of Hypersonic Boundary-Layer Flows," Air Force Office of Scientific Research, Contract F49620-88-C-0076, 16/May/88 - 15/May/91, Co-Principal Investigator with Helen Reed, $282,264, Responsible for $142,132.

"Effect of Sound on Boundary-Layer Stability," NASA Ames Research Center, Co-operative Agreement NCC2-659, 16/Nov/89 - 31/Jul/92, $94,106.

"Transition Receptivity and Control," Air Force Office of Scientific Research, Grant AFOSR-90-0234, 2/Jan/90 - 15/Dec/92, Co-Principal Investigator with Helen Reed, $353,391, Responsible for $222,580.

"Hybrid Laminar Flow Control Experiments in the NASA-Ames 11-foot Tunnel" NASA-Ames Research Center, University Consortium Interchange NCA2-745, 1/Sep/92 - 31/Mar/93, $11,893.

"Transition Studies on a Swept-Wing Model," NASA Langley Research Center, Grant NAG1-937, 1/Oct/88 - 15/May/94, $550,495.

Virginia Polytechnic Institute and State University

Principal or Co-Principal Investigator on research and equipment projects with sponsor totals of $2.0 million. Levels of responsibility on these projects total $1.4 million during nine years.

"Application of Stability Theory to Laminar Flow Control," NASA Langley Research Center, $180,000, A.H. Nayfeh and W.S. Saric - Co-Principal Investigators, 10/1/75 - 11/1/78. Responsible for $90,000.

"Experiments on the Stability and Transition of Two-Dimensional and Three-Dimensional Boundary Layers with Suction," NASA Langley Research Center, $127,000, W.S. Saric - Principal Investigator, 12/1/76 - 2/1/79. Responsible for $127,000.

"Experiments on the Nonparallel Stability of Boundary-Layer Flows," W.S. Saric and A.H. Nayfeh, National Science Foundation, $56,000, W.S. Saric - Principal Investigator, 2/15/78 - 5/1/79. Responsible for $56,000.

"Experiments to Verify Nonparallel Stability Theory," NASA Langley Research Center, $293,000, W.S. Saric - Principal Investigator, 4/1/79 - 1/15/83. Responsible for $293,000.

"Application of Nonlinear Stability Techniques to Boundary-Layer Transition," Naval Surface Weapons Center, White Oak, $31,938, W.S. Saric and Th. Herbert - Principal Investigators, 7/1/81 - 5/1/82. Responsible for $8,500.

"Aspects of Transition in Low-Reynolds-Number Aerodynamics," Office of Naval Research, $67,431, Th. Herbert and W.S. Saric - Principal Investigators, 1/1/83 - 12/15/83. Responsible for $33,700.


"Experiments on the Three-Dimensional Structure of Boundary Layers Undergoing Transition to Turbulence," A.F.O.S.R., $117,000, W.S. Saric - Principal Investigator, 6/1/82 - 12/15/83. Responsible for $117,000.

"An Analysis of Wave Interactions in Swept-Wing Flows," NASA Langley Research Center, $61,427, W.S. Saric and H.L. Reed - Principal Investigators, 10/7/82 - 1/31/84. (Joint with Stanford University.) Responsible for $27,900.

"Experiments on the 3-D Interactions of Disturbances in Boundary Layers," NASA Langley Research Center, $171,000, W.S. Saric - Principal Investigator, 6/1/82 - 9/15/84. Responsible for $171,000.

"An Analysis of the Nonlinear Stability of Circular Couette Flow," U.S. Army Research Office, $109,816, Th. Herbert and W.S. Saric - Principal Investigators, 6/16/82 - 6/15/84. Responsible for $12,000.

"High Reynolds Number, Flat-Plate Experiments in the National Transonic Facility," NASA Langley Research Center, $114,624, W.S. Saric - Principal Investigator, 7/26/82 - 7/25/84. Responsible for $114,624.

"Nonlinear Mechanisms in Unstable Plane Poiseuille Flow," National Science Foundation, $132,618, Th. Herbert and W.S. Saric - Principal Investigators, 10/16/82 - 8/31/84. Responsible for $30,000.

"Aspects of Low-Reynolds-Number Aerodynamics," Office of Naval Research, $160,000, Th. Herbert, J.F. Marchman and W.S. Saric, Principal Investigators, 12/15/83 - 8/31/84. Responsible for $75,100.

"On the Three-Dimensional Structure of Boundary Layers Undergoing Transition to Turbulence," A.F.O.S.R., $93,041, W.S. Saric and Th. Herbert, Principal Investigators, 2/16/84 - 8/31/84. Responsible for $60,000.

"432/CDS-VAX11/750 System for DoD University Research Instrumentation Program," Office of Naval Research, $263,903, W.S. Saric, D.P. Telionis, E.G. Henneke, and K.L. Reifsnider, Principal Investigators, 7/25/83 - 7/24/84. Responsible for $164,000.

resume of william s. saric 1 education ...kswt.tamu.edu/files/resumes/ws_resume.pdfresume of william...

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