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Flexible case analysis for compressible solid propellant grain motors Status reportStiffness version of finite element method used for numerical analysis of small elementary regions of solid propellant grains
Document ID
19660021325
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Key, S. W. (Mathematical Sciences Corp. Seattle, WA, United States)
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Subject Category
Propellants
Report/Patent Number
MSC-66-21-1
NASA-CR-76229
Report Number: MSC-66-21-1
Report Number: NASA-CR-76229
Accession Number
66N30615
Funding Number(s)
CONTRACT_GRANT: NAS7-242
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NUMERICAL ANALYSIS
PROPELLANT GRAIN
RITZ AVERAGING METHOD

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