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State of the art for panel flutter as applied to space shuttle heat shieldsSupersonic panel flutter of space shuttle heat shields with flexible supports
Document ID
19700027290
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Dixon, S. C. (NASA Langley Research Center Hampton, VA, United States)
Shore, C. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 5, 2013
Publication Date
July 1, 1970
Publication Information
Publication: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970
Subject Category
Structural Mechanics
Accession Number
70N36606
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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