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Computation of stresses in triangular finite elementsStress calculations in linear thin shells of aeolotropic material using deflections obtained by finite element method
Document ID
19660021497
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Utku, S. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
June 15, 1966
Subject Category
Structural Mechanics
Report/Patent Number
JPL-TR-32-948
NASA-CR-76292
Report Number: JPL-TR-32-948
Report Number: NASA-CR-76292
Accession Number
66N30787
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STRESS CALCULATION
THIN WALLED SHELL

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