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HYPERSCHALL
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NASA Langley Research Center, Supersonic and Hypersonic Testing Capabilities
NASA Langley Experimental Aerothermodynamic Contributions to Slender and Winged Hypersonic Vehicles
Application of PLIF to Investigate the Hypersonic Wake of a LOFTID-Relevant Model at Mach 10
FLEET and PLIF Velocimetry Within A Mach 10 Hypersonic Air Flow
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
Road to Hypersonic Weapons: Technical Challenges and Emerging Opportunities
The Influence of Computer Architecture on Performance and Scaling for Hypersonic Flow Simulations
Hypersonic Missile Nonproliferation: Hindering the Spread of a New Class of Weapons
Life Cycle Cost Modeling of High-Speed Commercial Aircraft: Final Review - Executive Summary