Boundary Layer Transition and Trip Effectiveness on an Apollo Capsule in the JAXA High Enthalpy Shock Tunnel (HIEST) Facility
Author:
Affiliation:
1. NASA Johnson Space Center
2. NASA Ames Research Center
3. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0209
Reference10 articles.
1. Investigation of Hypersonic Double-Cone Flow Experiments at High Enthalpy in the LENS Facility
2. Effect of Chemical Reaction Rates on Aero-Heating Predictions of Re-Entry Flows
3. Effect of High-Enthalpy Air Chemistry on Stagnation Point Heat Flux
4. Apollo-Shaped Capsule Boundary Layer Transition at High-Enthalpy in T5
5. Aeroheating measurement of Apollo shaped capsule with boundary layer trip in the free-piston shock tunnel HIEST
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2. Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes;Journal of Spacecraft and Rockets;2019-03
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