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HYPERSCHALL
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keywords:(HYPERSCHALL)
Correction: Bluntness Parameter for Hypersonic Vehicle Design
Effects of Nose Bluntness on Hypersonic Transition over Ogive-Cylinder Forebodies
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
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
Hypersonic Boundary-Layer Disturbances on a Cooled, Slender Cone at Mach 6
Characterization of a Glow Discharge in a Tripped Hypersonic Boundary Layer
Local Piston Theory with Viscous Correction and Its Application
Studies on Unsteady Shock Interactions Near a Generic Scramjet Inlet
Boundary-Layer Thermochemical Analysis During Passive and Active Oxidation of Silicon Carbide
Characterization of Disturbance Resonance in Postshock of Blunt Body in Hypersonic Flow
Effect of Leading-Edge Bluntness on Shockwave–Boundary-Layer Interaction in a Scramjet Intake
Experimental Verification of a Modified Cylindrical Focused Laser Differential Interferometer
Simulation of Hypersonic-Shock-Wave–Laminar-Boundary-Layer Interaction over Blunt Fin