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A method for determining aerodynamic damping of the structural bending modes with application to the Apollo/Saturn 1 launch vehicleComparison of damping derivatives and wind tunnel data of structural bending modes of Saturn 1
Document ID
19700026453
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Meadows, M. T. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
September 27, 1963
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-65007
Report Number: NASA-TM-X-65007
Accession Number
70N35769
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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