Effect of Deceleration on Pressure Distribution Along a Slender Cone in Supersonic, Transonic, and Subsonic Flight
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Published:1961-02
Issue:2
Volume:28
Page:173-174
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ISSN:1936-9999
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Container-title:Journal of the Aerospace Sciences
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language:en
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Short-container-title:Journal of the Aerospace Sciences
Author:
Hsu C. T.1,
Anderson D. A.1
Affiliation:
1. Iowa State University, Ames, Iowa
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Cited by
1 articles.
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1. Tecnical Notes;ARS Journal;1961-09