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HYPERSCHALL
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keywords:(HYPERSCHALL)
NASA Langley Research Center, Supersonic and Hypersonic Testing Capabilities
Application of PLIF to Investigate the Hypersonic Wake of a LOFTID-Relevant Model at Mach 10
Instability Results for Cone-Cylinder-Flare and Cone-Flare Hypersonic Wind-Tunnel Configurations
Modal and Nonmodal Instabilities over Cone-Cylinder-Flare Hypersonic Wind-Tunnel Configurations
Flow Instabilities over Cone-Cylinder-Flare Hypersonic Wind-Tunnel Configuration
Boundary-Layer Instabilities over Cone-Cylinder-Flare Models at Hypersonic Speeds
The Influence of Computer Architecture on Performance and Scaling for Hypersonic Flow Simulations
Discrete Roughness Boundary-Layer Transition at Hypersonic Conditions
BOLT: Streak Instability Analysis (Including AoA and Yaw Effects)
Dynamic Force Reconstruction of Transient Flap Control Force Experiments in a Hypersonic Wind Tunnel