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An analysis of aeroelastic divergence in unguided launch vehiclesDiscrete system matrix method for analyzing aeroelastic divergence behavior of unguided slender body launch vehicles
Document ID
19660010197
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Alley, V. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Gerringer, A. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1964
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3281
Accession Number
66N19486
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MATRIX ANALYSIS
AEROELASTICITY
LAUNCH VEHICLE
SLENDER BODY

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