Aerodynamic Heating Measurement on Afterbody of Hypersonic Flight Experiment
Author:
Affiliation:
1. National Aerospace Laboratory, Chofu, Tokyo 182-8522, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3409
Reference12 articles.
1. Approximate Convective-Heating Equations for Hypersonic Flows
2. Boundary-layer transition on swept cylinders at hypersonic speeds
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