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Engineering estimates for supersonic flutter of curved shell segments.Cylindrical shell segments supersonic flutter boundaries engineering estimates related to Saturn 5 booster, obtaining thickness requirement as function of panel geometry
Document ID
19680043268
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, W. J.
Hsu, K.-H.
Date Acquired
August 4, 2013
Publication Date
April 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 68-284
Report Number: AIAA PAPER 68-284
Meeting Information
Meeting: STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE
Location: PALM SPRINGS, CA
Country: US
Start Date: April 1, 1968
End Date: April 3, 1968
Sponsors: AMERICAN SOCIETY OF MECHANICAL ENGINEERS, AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A24240
Funding Number(s)
CONTRACT_GRANT: NGR-23-005-166
Distribution Limits
Public
Copyright
Other

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