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Stress waves resulting from hypervelocity impact.Characteristics method for stress waves from hypervelocity impact of circular cylinder on half space, discussing numerical diffusion effect on pressure and flow fields
Document ID
19690050298
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chang, T. S.
Madden, R.
Date Acquired
August 5, 2013
Publication Date
April 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 69-355
Report Number: AIAA PAPER 69-355
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, HYPERVELOCITY IMPACT CONFERENCE
Location: CINCINNATI, OHIO
Start Date: April 30, 1969
End Date: May 2, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A28287
Funding Number(s)
CONTRACT_GRANT: NGR-34-002-084
CONTRACT_GRANT: N00014-68-A-0187
Distribution Limits
Public
Copyright
Other

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