Drag Reduction Studies by Steady Energy Deposition at Mach 5
Author:
Affiliation:
1. University of Manchester
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1027
Reference27 articles.
1. Blunt-Body Wave Drag Reduction Using Focused Energy Deposition
2. Preliminary Investigations of Spiked Bodies at Hypersonic Speeds
3. The flow of a jet from a body opposing a supersonic free stream
4. Jet-Spike Bifurcation in High-Speed Flows
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