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A simple method for determining the bending moment equation that includes vehicle elastic and sloshing modes and a numerical exampleBending moment of vehicle in terms of control parameters - vehicle elastic and sloshing modes
Document ID
19650014530
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ryan, R. S. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Swift, F. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Townsend, D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Structural Mechanics
Accession Number
65N24131
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT VEHICLE
BENDING MOMENT
ELASTIC BENDING
CONTROL STABILITY
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Related Records

IDRelationTitle19650014524Collected WorksAero-Astrodynamics Research and Development Research Review No. 1, January 1 - June 30, 1964
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