Formation of Bow Shock Waves Around a Blunt Body in Magnetohydrodynamics Flows
Author:
Affiliation:
1. Chinese Academy of Sciences, 100190 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35315
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1. Boundary Layer Transition Flight Experiment Overview
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5. A study of performance parameters on drag and heat flux reduction efficiency of combinational novel cavity and opposing jet concept in hypersonic flows
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