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Inelastic, nonlinear analysis of stiffened shells of revolution by numerical integrationThis paper describes the latest addition to the STARS system of computer programs, STARS-2P, for the plastic, large deflection analysis of axisymmetrically loaded shells of revolution. The STARS system uses a numerical integration scheme to solve the governing differential equations. Several unique features for shell of revolution programs that are included in the STARS-2P program are described. These include orthotropic nonlinear kinematic hardening theory, a variety of shell wall cross sections and discrete ring stiffeners, cyclic and nonproportional mechanical and thermal loading capability, the coupled axisymmetric large deflection elasto-plastic torsion problem, an extensive restart option, arbitrary branching capability, and the provision for the inelastic treatment of smeared stiffeners, isogrid, and waffle wall constructions. To affirm the validity of the results, comparisons with available theoretical and experimental data are presented.
Document ID
19740050691
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Levine, H. S.
Svalbonas, V.
(Grumman Aerospace Corp. Bethpage, N.Y., United States)
Date Acquired
August 7, 2013
Publication Date
May 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
ASME PAPER 74-PVP-35
Accession Number
74A33441
Funding Number(s)
CONTRACT_GRANT: NAS8-28569
Distribution Limits
Public
Copyright
Other

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