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The Calculation of the Bending Moment Response of a Typical Launch Vehicle Using Generalized Power Spectral TechniquesBending moment response calculation of launch vehicle using generalized power spectral techniques
Document ID
19660014456
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Beer, F. P. (Lehigh Univ. Bethlehem, PA, United States)
Lennox, W. C. (Lehigh Univ. Bethlehem, PA, United States)
Date Acquired
August 3, 2013
Publication Date
February 15, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-74386
Report Number: NASA-CR-74386
Accession Number
66N23745
Funding Number(s)
CONTRACT_GRANT: NSG-466
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LAUNCH VEHICLE
BENDING MOMENT
POWER SPECTRUM

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