Investigation of Missile-Shaped Body with Forward-Facing Cavity at Mach 8
Author:
Affiliation:
1. Indian Institute of Science, Bangalore 560 012, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.38914
Reference30 articles.
1. Experimental Investigations of Hypersonic Flow over Highly Blunted Cones with Aerospikes
2. Effect of concentrated energy deposition on the aerodynamic drag of a blunt body in hypersonic flow
3. Film cooling effectiveness on a large angle blunt cone flying at hypersonic speed
4. Mach 10 bow-shock behavior of a forward-facing nose cavity
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