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Computer program for stresses and buckling of heated composite-stiffened panels and other structures (BUCLASP 3)General-purpose program is intended for thermal stress and instability analyses of structures such as axially-stiffened curved panels. Two types of instability analyses can be effected by program: (1) thermal buckling with temperature variation as specified and (2) buckling due to in-plane biaxial loading.
Document ID
19740000204
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Viswanathan, A. V. (Boeing Co.)
Tamekuni, M. (Boeing Co.)
Tripp, L. L. (Boeing Co.)
Date Acquired
August 7, 2013
Publication Date
November 1, 1974
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LAR-11533
Accession Number
74B10204
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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