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Acoustic Analysis of Solid Rocket Motor Cavities by a Finite Element MethodAdaptation of NASTRAN program to solve acoustic mode problems of solid rocket motor cavities by finite element method
Document ID
19710026795
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Herting, D. N. (MacNeal-Schwendler Corp. San Marino, CA, United States)
Joseph, J. A. (MacNeal-Schwendler Corp. San Marino, CA, United States)
Kuusinen, L. R. (MacNeal-Schwendler Corp. San Marino, CA, United States)
Macneal, R. H. (MacNeal-Schwendler Corp. San Marino, CA, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1971
Publication Information
Publication: NASA. Langley Res. Center NASTRAN: Users Experiences
Subject Category
Propulsion Systems
Accession Number
71N36271
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19710026777Collected WorksNASTRAN: Users' Experiences
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