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AN AEROELASTIC MODEL APPROACH FOR THE PREDICTION OF BUFFET BENDING LOADS ON LAUNCH VEHICLESAeroelastic model approach for prediction of buffet bending loads on launch vehicles
Document ID
19630013802
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Doggett, R. V., Jr. (NASA Langley Research Center Hampton, VA, United States)
Hanson, P. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2022
Report Number: NASA-TN-D-2022
Accession Number
63N23682
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BUFFETING
AEROELASTICITY
LAUNCH VEHICLE

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