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Axisymmetric thermal stresses in sandwich shells of revolution with application to shallow, spherical shellsAxisymmetric thermal stresses in sandwich shells of revolution with application to shallow spherical shells
Document ID
19660022376
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Williams, H. E. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
July 15, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-76428
JPL-TR-32-920
Report Number: NASA-CR-76428
Report Number: JPL-TR-32-920
Accession Number
66N31666
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AXISYMMETRIC DEFORMATION
THERMAL STRESS
BENDING MOMENT
SPHERICAL SHELL
SHELL STABILITY

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