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In plane stress analysisAn investigation of the blowing up of UK numerical results for the inplane stress calculations for silicon ribbon is presented. The inplane stress that exists in a thin plate is governed by two general equations of equilibrium and compatibility.
Document ID
19850018948
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dillon, O. W., Jr. (Kentucky Univ. Lexington, KY, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1985
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-175775
DOE/JPL-956571-85/02
NAS 1.26:175775
Report Number: NASA-CR-175775
Report Number: DOE/JPL-956571-85/02
Report Number: NAS 1.26:175775
Accession Number
85N27259
Funding Number(s)
CONTRACT_GRANT: JPL-956571
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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