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Hypersonic
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tunnels
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NASA Langley Research Center, Supersonic and Hypersonic Testing Capabilities
Experimental and numerical investigation for hypersonic performance of double swept waverider
Flow-Based Prediction for Self-Starting Limit of Two-Dimensional Hypersonic Inlets
Ground experimentation with 3D printed scramjet inlet models at hypervelocities
Experimental study of hypersonic traveling crossflow instability over a yawed cone
Introduction to the Special Section on the Boundary Layer Transition (BOLT) Flight Experiment
Tomographic Reconstruction of Hypersonic Aircraft Flowfields in Large-Scale Wind Tunnel Experiments
Pursuit of Power : NASA's Propulsion Systems Laboratory No. 1 and 2
Measurement and analysis of crossflow instability modes on a 7-degree yawed cone at Mach 6
Typical model design to measure aerodynamic coefficients in the presence of supersonic plume
Open Rotor Research at NASA Glenn
Nonlinear Instability Characterization of Hypersonic Laminar Boundary Layer
Analysis of Associative Ionization Rates for Hypersonic Flows
Wall Pressure Fluctuations Beneath Hypersonic Boundary Layer over Plate
Variable geometry cowl sidewall for improving rectangular hypersonic inlet performance
Similarity and Key Parameters of Retropropulsion Assisted Deceleration in Hypersonic Wind Tunnels