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Manual for Program PSTRESS: Peel stress computationDescribed is the use of the interactive FORTRAN computer program PSTRESS, which computes a closed form solution for two bonded plates subjected to applied moments, vertical shears, and in-plane forces. The program calculates in-plane stresses in the plates, deflections of the plates, and peel and shear stresses in the adhesive. The document briefly outlines the analytical method used by PSTRESS, describes the input and output of the program, and presents a sample analysis. The results of the latter are shown to be within a few percent of results obtained using a NASTRAN finite element analysis. An appendix containing a listing of PSTRESS is included.
Document ID
19900002506
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barkey, Derek A.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Madan, Ram C.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1987
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-178408
NAS 1.26:178408
Accession Number
90N11822
Funding Number(s)
CONTRACT_GRANT: NAS1-17970
PROJECT: RTOP 505-63-11-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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