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Diffraction of shock wave by moving thin wing.Flow field pressure distribution due to plane shock wave impinging by thin wing moving in opposite direction, discussing mathematical formulation, analytic solution and applications
Document ID
19690055470
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gunzburger, M.
Ting, L.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 69-647
Report Number: AIAA PAPER 69-647
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, FLUID AND PLASMA DYNAMICS CONFERENCE
Location: SAN FRANCISCO, CALIF.
Start Date: June 16, 1969
End Date: June 18, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A33459
Funding Number(s)
CONTRACT_GRANT: NGR-33-016-119
Distribution Limits
Public
Copyright
Other

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