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Buckling loads of stiffened panels subjected to combined longitudinal compression and shear: Results obtained with PASCO, EAL, and STAGS computer programsBuckling analyses used in PASCO are summarized with emphasis placed on the shear buckling analyses. The PASCO buckling analyses include the basic VIPASA analysis, which is essentially exact for longitudinal and transverse loads, and a smeared stiffener solution, which treats a stiffened panel as an orthotropic plate. Buckling results are then presented for seven stiffened panels loaded by combinations of longitudinal compression and shear. The buckling results were obtained with the PASCO, EAL, and STAGS computer programs. The EAL and STAGS solutions were obtained with a fine finite element mesh and are very accurate. These finite element solutions together with the PASCO results for pure longitudinal compression provide benchmark calculations to evaluate other analysis procedures.
Document ID
19840008517
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Stroud, W. J.
(NASA Langley Research Center Hampton, VA, United States)
Greene, W. H.
(NASA Langley Research Center Hampton, VA, United States)
Anderson, M. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.60:2215
L-15630
NASA-TP-2215
Accession Number
84N16585
Funding Number(s)
PROJECT: RTOP 534-03-23-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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