An Investigation of the Detached Shock in Front of a Body of Revolution
Author:
Affiliation:
1. Grumman Aircraft Engineering Corporation,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.11698
Reference5 articles.
1. On the Flow Behind Curved Shocks
2. Ladenburg, R., Van Voorhis, C. C , and Winkler, J., Interferometric Study of Supersonic Phenomena, NAVORD Reports 69-46 (Part I), 93-46 (Part II), 7-47 (Part I I I ) .
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2. Series solution for the planar asymmetric blunt-body problem;Physics of Fluids;1975
3. Hypersonic flows generated by parabolic and paraboloidal shock waves;Physics of Fluids;1974
4. A REVIEW OF SOME RECENT DEVELOPMENTS IN HYPERSONIC FLOW**This work was supported by the United States Air Force through the Office of Scientific Research, Air Research and Development Command, under Contract AF 49 (638)-217, and through the Aeronautical Research Laboratory of Wright Air Development Center, under Contract No. 33 (616)-3265.;Advances in Aeronautical Sciences;1959
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