capt barry croker executive officer to the afrl vice commander air force research laboratory
DESCRIPTION
ON THE DESIGN OF HYPERSONIC INLETS 3rd Symposium on Integrating CFD & Experiments in Aerodynamics USAFA, CO 20-21 June, 2007. Capt Barry Croker Executive Officer to the AFRL Vice Commander Air Force Research Laboratory. Acknowledgements. - PowerPoint PPT PresentationTRANSCRIPT
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ON THE DESIGN OF HYPERSONIC INLETS
3rd Symposium on Integrating CFD & Experiments in Aerodynamics
USAFA, CO
20-21 June, 2007
Capt Barry CrokerExecutive Officer to the AFRL Vice Commander
Air Force Research Laboratory
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Acknowledgements
• Dr. Datta GaitondeMs. Heidi MeicenheimerMr. Pete KutschenreuterAir Vehicles Directorate, AFRL
• Dr. John SchmisseurAFOSR
• DoD HPCMO, ASC MSRC
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Overview
• USAF High Speed Vision
• Hypersonic Design Process
• JAWS Inlet Program
– Design Methodology
– CFD Verification & Validation
– Experimental Test Program
• Conclusions
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Future Capabilities: Prompt Global StrikeLong Range StrikeOperationally Responsive Access to Space
USAF High Speed Mission
Hypersonic flight will enable unparalleled global reach and power
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Balance engine/airframeover entire speed regime
Cowl lip dragand heat transfer
Boundary layertransition on external surfaces and inlet
Fuel injection drag,mixing and heat transfer
Nozzle over-expansionat transonic speeds
External burning ignitionand flame-holding
Mass capture, contractionlimits in inlet
Nozzle recombinationlosses
Isolator performanceand operability
Shock/boundary layerinteractions
Challenges of High Speed Flight
Key enabling technologies need to be developed to make sustained hypersonic flight feasible!
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AFRL Design Core Competency
EngineeringDesign Tools
High-FidelityCFD
ExperimentalGround Testing
“…to establish a core-competency in hypersonic vehicle inlet design…”
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Engineering Design
X
Y
Z
0
2
R
X 1
X 2
Y0
b
4
SHOCK BOX
1
2
1
2
R
Y1
Y0
X1
UPSTREAM X-Y PLANE
3
4
3
4
R
Z4
b
X2
DO W NSTREAM X-Z PLANE
Invisicid Streamtracing
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Computational Verification
AVUSDesign Space Exploration2nd Order Unstructured RANS + SA or BL
FDL3DIHigh-Fidelity Analysis3rd Order Structured RANS + k-
EulerStream Trace VerificationShock Location
TurbulentViscous CorrectionsNonlinear Effects
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Centerline X-Y Plane
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2D Centerline X-Y Plane
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2D Centerline X-Y Plane
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JAWS
Inward-Turning, Circular Cross Section M = 5 - 10Q = 1000-1500 psf
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Planar Shock Topology
X
Z
Y
Quarter-SectionRectangular Analogy
Full Topology
Primary Shock
Primary Reflection
Secondary Shock
Secondary Reflection
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Inviscid Results
Mach Number along X-Z Centerline Plane
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Inviscid Results
Mach Number along X-Y Centerline Plane
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Viscous Correction
JAWS3 Windtunnel Model - Inviscid/Viscous
0.0
0.5
1.0
1.5
0.0 0.5 1.0 1.5
Z - Inches
Y -
In
ches
Lip
Shk2 Impingement
Shk4 Impingement & Exit
Viscous Shk2 Impingement
Viscous exit
Boundary layer momentum thickness accounted for through each shock
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Turbulent Results
Mach Number along X-Y Centerline Plane
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Turbulent Results
Mach Number along X-Z Centerline Plane
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Comparison of Results
Invisicid
Viscous
Mach Number along X-Y Centerline Plane
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Comparison of Results
Invisicid Viscous
Mach Number at Exit Plane
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Swept-Shock Boundary Layer Interaction
Isosurface of TKE in Boundary Layer
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Swept-Shock Boundary Layer Interaction
• Separated Boundary Layer• Centerline Vortex• Interaction Flows
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Conclusions of CFD
Overall shock structure well aligned with prediction
Viscous correction adequate for shock location
Influence of Swept-Shock Boundary Layer Interaction could have implications on performance
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Experimental Test Program
• NASA Langley Aerothermodynamics Branch 20” Mach 6 Tunnel
• Originally Planned for May, Slipped to August
• Test Goals:
– Establish inlet starting parameters
– Back-pressure study
– Evaluate on and off design performance
• Angle of Attack/Yaw
• Re & Minf
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Model Fabrication
• Instrumentation location based on CFD predictions
• Diagnostics include:- Pressure- Temperature- Surface Oil Flow Visualization
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Conclusions & Future Work
• Functional Analytical Design
• CFD to check & improve method
• EFD to verify computations & improve method
• CFD on off-design cases
• Comparison of CFD & EFD data
EngineeringDesign Tools
High-FidelityCFD
ExperimentalGround Testing