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Computer program provides improved longitudinal response analysis for axisymmetric launch vehiclesComputer program calculates axisymmetric launch vehicle steady-state response to axisymmetric sinusoidal loads. A finite element technique is utilized to construct the total launch vehicle stiffness matrix and mass matrix by subdividing the prototype structure into a set of axisymmetric shell components, fluid components, and spring-mass components.
Document ID
19670000530
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Smith, W. W.
Walton, W. C., Jr.
Date Acquired
August 3, 2013
Publication Date
December 1, 1967
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LAR-10093
Report Number: LAR-10093
Accession Number
67B10531
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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