Experimental Study of High-Enthalpy Heat Flux Augmentation in Shock Tunnels
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Kakuda, Miyagi 9811525, Japan
2. NASA Johnson Space Center, Houston, Texas 77058
3. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.T4478
Reference9 articles.
1. Computational Modeling of T5 Laminar and Turbulent Heating Data on Blunt Cones, Part 1: Titan Applications
2. Apollo-Shaped Capsule Boundary Layer Transition at High-Enthalpy in T5
3. Assessment of Laminar, Convective Aeroheating Prediction Uncertainties for Mars Entry Vehicles
4. Hypersonic aerothermodynamic and scramjet research using high enthalpy shock tunnel
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