Aeroheating measurements on a reentry capsule model in free-piston shock tunnel HIEST
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1181
Reference17 articles.
1. Hypersonic aerothermodynamic and scramjet research using high enthalpy shock tunnel
2. 2Tanno.H.,et.al."HeatFluxMeasurementofApolloCapsuleModelintheFree-PistonShockTunnelHIEST ",AIAAPaper No.2009-7304, 2009.
3. Transient heat flux measurement using a surface junction thermocouple
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