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Study of propellant dynamics in a shuttle type launch vehicleA method and an associated digital computer program for evaluating the vibrational characteristics of large liquid-filled rigid wall tanks of general shape are presented. A solution procedure was developed in which slosh modes and frequencies are computed for systems mathematically modeled as assemblages of liquid finite elements. To retain sparsity in the assembled system mass and stiffness matrices, a compressible liquid element formulation was incorporated in the program. The approach taken in the liquid finite element formulation is compatible with triangular and quadrilateral structural finite elements so that the analysis of liquid motion can be coupled with flexible tank wall motion at some future time. The liquid element repertoire developed during the course of this study consists of a two-dimensional triangular element and a three-dimensional tetrahedral element.
Document ID
19730009074
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jones, C. E.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Feng, G. C.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1972
Subject Category
Propellants
Report/Patent Number
LMSC/HREC-D225823
HREC-7012-1
NASA-CR-124070
Report Number: LMSC/HREC-D225823
Report Number: HREC-7012-1
Report Number: NASA-CR-124070
Accession Number
73N17801
Funding Number(s)
CONTRACT_GRANT: NAS8-27012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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