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Mach-Zahl
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Numerical exploration of dissimilar supersonic coaxial jets mixing
Shock train behavior affected by continuous Mach number variation of incoming flow
The influence of compressibility on the aerodynamics of an inverted wing in ground effect
Prediction of the Wind Tunnel Sidewall Effect for the iGREEN Wing-Tailplane Interference Experiment
Experimental investigation of diaphragm material combinations in a small-scale shock tube
Characterization of a high-frequency pulsed-plasma jet actuator for supersonic flow control
Computation of Trailing Edge Noise with a Discontinuous Galerkin Method
Turbine-based combined cycle propulsion system integration concept design
Hydrogen tube vehicle for supersonic transport: Analysis of the concept
Yaw Stability Analysis for UiTM's BWB Baseline-II UAV E-4
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
Fuel Consumption Due to Shaft Power Off-Takes from the Engine
Fuel consumption due to shaft power off-takes from the engine
A combined PIV/force balance study of a fin-wake aerodynamic interaction
Prediction of aerodynamic noise reduction by using open-cell metal foam
Effect of endwall vortex generator jets on flow separation control in a linear compressor cascade
Vibration response of spacecraft shrouds to in-flight fluctuating pressures
Investigation of Transient Shock Wave in Supersonic Wind Tunnel
Propeller noise reduction by means of unsymmetrical blade-spacing
Aerodynamische Modelle aus Erbiumoxid in Überschallströmungen
Velocity scaled aeroelastic testing of advanced turboprops
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
Effect of inlet conditions on compressor intermediate duct
Hysteresis phenomenon of hypersonic inlet at high Mach number
Aerodynamic optimization under a range of operating conditions
Longitudinal Aerodynamics of a Canard Guided Spin Stabilized Projectile
Optimization of dielectric barrier discharge plasma actuators for active aerodynamic flow control
Landing-gear noise prediction using high-order finite difference schemes
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
The Effect of Canard to the Aerodynamic Behavior of Blended Wing Body Aircraft