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Application of recent panel flutter research to the space shuttle. Part 2 - Influence of edge clips and flow angularityParameters contributing to aeroelastic problems in thermal protection of space shuttle
Document ID
19710015185
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bohon, H. L. (NASA Langley Research Center Hampton, VA, United States)
Shore, C. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Publication Information
Publication: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 3 APR. 1971
Subject Category
Structural Mechanics
Accession Number
71N24661
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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