Computational Analyses to Support Design of Hollow Cylinder Flare Experiments at AEDC Hypervelocity Tunnel 9
Author:
Affiliation:
1. Johns Hopkins University Applied Physics Laboratory
2. Office of Naval Research
3. Arnold Engineering Development Complex
Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Review of the physics of swept-shock/boundary layer interactions
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4. CFD validation for hypersonic flight - Hypersonic double-cone flow simulations
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