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Test Facilities of the Dfvlr in the Transonic and Hypersonic Speed Range and Main Activities
Test-Facilities of the Dfvlr in the Transonic and Hypersonic Speed-Range and Main Activities
Wind Tunnels. January, 1976-January, 1981 (Citations from the Energy Data Base)
Second-Mode Measurements at High Reynolds Numbers
Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy
Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Large-Scale Hypersonic Facility
Shock Train/Boundary-Layer Interaction in Rectangular Isolators
Supersaturation Total Temperature, Pitot Pressure, and Rayleigh Scattering Measurements at Mach 10
Ffa Wind Tunnel Facilities. Part 3 - Hypersonic Tunnels
Direct Numerical Simulation Database for Supersonic and Hypersonic Turbulent Boundary Layers
PRODUCTION AND DIAGNOSTICS OF HYPERVELOCITY LOW-DENSITY STREAMS
Disturbance Level Characterization of a Hypersonic Blowdown Facility
Nose-Tip Bluntness Effects on Transition at Hypersonic Speeds
Nonintrusive Freestream Velocity Measurement in a Large-Scale Hypersonic Wind Tunnel
Prediction Methodology for Second-Mode-Dominated Boundary-Layer Transition in Wind Tunnels
APOLLO Command Module Aerodynamic Simulation Test in Hypersonic Flow
APOLLO Command Module Aerodynamic Simulation Test in Hypersonic Flow
The Test Section of the Wind Tunnel for Jet Propulsion Research of the Dfvlr at Trauen
Nose-Tip Bluntness Effects on Transition at Hypersonic Speeds
Hypersonic Low Density Wind Tunnel Plant
Hypersonic Aerothermal Characteristics of a Manned Low Finenes Ratio Shuttle Booster
Energy addition methods for hyper-velocity true flight simulation
Analysis of Second-Mode Amplitudes on Sharp Cones in Hypersonic Wind Tunnels
Investigation of a Liquid Nitrogen Cooled Nozzle of the Hypersonic Low Density Wind Tunnel
Calibration of a Mach 7 Nozzle for the First Test Section of the Ava Hypersonic Wind Tunnel
Assessment of Productive Computational Fluid Dynamics for Aerodynamic Design
Transition Prediction in Hypersonic Boundary Layers Using Receptivity and Freestream Spectra
Direct Skin Friction Measurements at Mach 10 in a Hypervelocity Wind Tunnel
Direct Skin Friction Measurements at Mach 10 in a Hypervelocity Wind Tunnel
Experimental Investigations on Wave Riders (Caret Wings) in the Hypersonic Range