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HYPERSCHALL
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keywords:(HYPERSCHALL)
Parametric aero-thermo-mechanical investigation of a hypersonic transport glider
Numerical Investigation of a Generic Scramjet Configuration
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow
Correction: Bluntness Parameter for Hypersonic Vehicle Design
Review of acoustic metasurfaces for hypersonic boundary layer stabilization
Actes du Symposium Européen sur l'Avenir du Transport Aérien à Haute Vitesse
Actes du Symposium Européen sur l'Avenir du Transport Aérien à Haute Vitesse
Effects of Nose Bluntness on Hypersonic Transition over Ogive-Cylinder Forebodies
Aerodynamic and aerothermodynamic design of Future Launchers Preparatory Program concepts
Research on hypersonic aircraft using pre-cooled turbojet engines
Design of an Internal Osculating Waverider Intake
Flow-Based Prediction for Self-Starting Limit of Two-Dimensional Hypersonic Inlets
Wall Pressure Fluctuations Beneath Hypersonic Boundary Layer over Plate
Separation process of multi-spheres in hypersonic flow
Experimental study of separation behavior of two bodies in hypersonic flow
Spezialgebiete der Gasdynamik : Schallnähe, Hyperschall, Tragflächen, Wellenausbreitung
Numerical investigation of combustion field of hypervelocity scramjet engine
Experimental and numerical study on the local unstart mechanism of hypersonic inlet
Air–Carbon Ablation Model for Hypersonic Flight from Molecular-Beam Data
Acoustic Properties of Porous Coatings for Hypersonic Boundary-Layer Control
Analysis of Associative Ionization Rates for Hypersonic Flows
Reliability analysis for a hypersonic aircraft’s wing spar
Hypersonic Boundary-Layer Disturbances on a Cooled, Slender Cone at Mach 6
NASA Langley Research Center, Supersonic and Hypersonic Testing Capabilities
Characterization of a Glow Discharge in a Tripped Hypersonic Boundary Layer
Technology roadmapping methodology for future hypersonic transportation systems
NASA Langley Experimental Aerothermodynamic Contributions to Slender and Winged Hypersonic Vehicles
Local Piston Theory with Viscous Correction and Its Application
Aerodynamic performance investigation on waverider with variable blunt radius in hypersonic flows
A study on heat flux predictions for re-entry flight analysis