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Waves
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keywords:(Mach Waves)
XB-70 Pilot Flight Report Flight 1-17 14 OCTOBER 1965
Wedge-Induced Oblique Detonations with Small Heat Release
Wave-Packet Representation of Shock-Cell Noise for a Single Round Jet
Wave Loading on Vertical Sheet-Pile Groins and Jetties
Wall Temperature and Suction Control of Linear Modes in Compressible Corner Flow
Vortex Generators for Corner Separation Caused by Shock-Wave/Boundary-Layer Interactions
Upstream Influence in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8
Unsteady Supersonic Flow for a Plate Undergoing Three-Stage Sinking Motion
Uncertainty and Sensitivity Analysis of Bleed Modeling in Shock/Turbulent Interactions
Transition induced by distributed roughness on blunt bodies in supersonic flow
Transition Between Different Initiation Structures of Wedge-Induced Oblique Detonations
Toward New Horizons. Volume 4. Aerodynamics and Aircraft Design
Toward a Comprehensive Model of Jet Noise Using an Acoustic Analogy
Three-Way Spectral Decompositions of High-Performance Military Aircraft Noise
Thermal Performance of Transonic Cooled Tips in a Turbine Cascade
THE NUMERICAL CALCULATION OF PLANE STEADY TRANSONIC FLOWS PAST LIFTING AIRFOILS
Temperature Effects on Convection Speed and Steepened Waves of Temporally Developing Supersonic Jets
Supersonic Turbulent Boundary-Layer Separation Control Using a Morphing Surface