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Asymptotic theory of the pressure on a cylindrical shell performing unsteady oscillation in external or internal supersonic flow
[Place of publication not identified] : [publisher not identified], 1968.
pages " 503, 857, -510, 864"
American Institute of Aeronautics and Astronautics. Technical Information Service
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Abstracted in International Aerospace Abstracts.
Reproduced from: Academie Polonaise Des Sciences, Bulletin, Serie Des Sciences Techniques
Microform. New York : American Institute of Aeronautics and Astronautics, Technical Information Service, [19--?]
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| catkey: 19132342