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Engineering estimates for supersonic flutter of curved shell segmentsCylindrical shell segments supersonic flutter boundaries engineering estimates related to Saturn 5 booster, obtaining thickness requirement as function of panel geometry
Document ID
19700049843
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Anderson, W. J.
Hsu, K.-H.
Date Acquired
August 5, 2013
Publication Date
March 1, 1970
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 68-284
Report Number: AIAA PAPER 68-284
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AND AMERICAN SOCIETY OF MECHANICAL ENGINEERS, STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE, 9TH
Location: PALM SPRINGS, CA
Start Date: April 1, 1968
End Date: April 3, 1968
Sponsors: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A25959
Distribution Limits
Public
Copyright
Other

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