Drag Reduction Using Aerodisks for Hypersonic Hemispherical Bodies
Author:
Affiliation:
1. University of Sheffield, Sheffield S1 3JD, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.46655
Reference28 articles.
1. Experimental Investigations of Hypersonic Flow over Highly Blunted Cones with Aerospikes
2. Experimental investigation on spiked body in hypersonic flow
3. Experimental studies of separated flows at hypersonic speeds. I - Separated flows over axisymmetric spiked bodies.
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