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Mach-Zahl
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Numerical exploration of dissimilar supersonic coaxial jets mixing
The influence of compressibility on the aerodynamics of an inverted wing in ground effect
Shock train behavior affected by continuous Mach number variation of incoming flow
Characterization of a high-frequency pulsed-plasma jet actuator for supersonic flow control
Experimental investigation of diaphragm material combinations in a small-scale shock tube
Turbine-based combined cycle propulsion system integration concept design
Hydrogen tube vehicle for supersonic transport: Analysis of the concept
Numerical study on hypersonic nozzle-inlet starting characteristics in a shock tunnel
Effects of hypersonic vehicle's optical dome on infrared imaging
Comment on “Acoustic Velocity Formulation for Sources in Arbitrary Motion”
Behaviour of turbulent Prandtl/Schmidt number in compressible mixing layer
Prediction of aerodynamic noise reduction by using open-cell metal foam
Vibration response of spacecraft shrouds to in-flight fluctuating pressures
Effect of endwall vortex generator jets on flow separation control in a linear compressor cascade
Aerodynamic optimization under a range of operating conditions
Propeller noise reduction by means of unsymmetrical blade-spacing
Effect of inlet conditions on compressor intermediate duct
Roll control feasibility of a slender cruciform configuration by canard surfaces at Mach number 2.25
Exhaust Gas and Plume Modeling Effects for Space Launch System Abort Scenarios
Hysteresis phenomenon of hypersonic inlet at high Mach number
Landing-gear noise prediction using high-order finite difference schemes
Optimization of dielectric barrier discharge plasma actuators for active aerodynamic flow control
Buzz Characteristics Under Fluid–Structure Interaction of Variable-Geometry Lip for Hypersonic Inlet
An analytical approach for stand-off distance of detached shock waves
Investigation of crossflow shocks on delta wings in supersonic flow
An overview of research on wide-speed range waverider configuration
Extremizing feedback control of a high-speed and high Reynolds number jet
Fast Fourier Transformation Computation of Modal Transfer Function for Rotating Source Localization
The joint international R & D project on hypersonic transport propulsion system (HYPR project)
Turbulence model behavior in low Reynolds number regions of aerodynamic flowfields
Experimental and simulation testing of flight spin stability for small caliber cannon projectile
Jet engine exhaust noise due to rough combustion and nonsteady aerodynamic sources
Rotating co-flow jets with horizontal lip and shape transition
Flight simulation characteristics of the Langley high Reynolds number cryogenic transonic tunnel
The Mach number prediction based on the feature subsets ensemble in transonic wind tunnel
Mach number dependence of the compression wave generated by a high-speed train entering a tunnel