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Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design
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Flow separation in shock wave boundary layer interactions at hypersonic speeds
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Shock-tunnel combustor testing for hypersonic vehicles
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Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis
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Transition at hypersonic speeds
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Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
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Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
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Computational study of flow establishment in hypersonic pulse facilities
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Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
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Mach 6 flow field surveys beneath the forebody of an airbreathing missile
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Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements
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Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program
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Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF
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Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
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Physics of interplanetary dust collection with aerogel
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Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
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Hypersonic flows as related to the national aerospace plane
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Parametric study of shock-induced combustion in a hydrogen air system
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On the Gortler vortex instability mechanism at hypersonic speeds
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Multiphysics simulation of active hypersonic lip cooling
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Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
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Mach 10 computational study of a three-dimensional scramjet inlet flow field
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Application of CFD to the analysis and design of high-speed inlets
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Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
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