scholarly journals Numerical integration of large deflection elastic--plastic axisymmetric shells of revolution

1976 ◽  
Author(s):  
H. Ahmed
1974 ◽  
Vol 96 (2) ◽  
pp. 121-130 ◽  
Author(s):  
H. S. Levine ◽  
V. Svalbonas

This 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.


1972 ◽  
Vol 15 (85) ◽  
pp. 796-804 ◽  
Author(s):  
Yoshio ANDO ◽  
Kunihiro IIDA ◽  
Tadahiko KAWAI ◽  
Genki YAGAWA ◽  
Fumio KIKUCHI

AIAA Journal ◽  
1971 ◽  
Vol 9 (6) ◽  
pp. 1012-1018 ◽  
Author(s):  
J. C. GERDEEN ◽  
F. A. SlMONEN ◽  
D. T. HUNTER

1974 ◽  
Vol 96 (2) ◽  
pp. 87-95 ◽  
Author(s):  
J. A. Stricklin ◽  
W. E. Haisler ◽  
W. A. Von Riesemann

This paper presents the formulation and check-out problems for a computer code DYNAPLAS, which analyzes the large deflection elastic-plastic dynamic response of stiffened shells of revolution. The formulation for spacial discretization is by the finite element method with finite differences being used for the evaluation of the pseudo forces due to material and geometric nonlinearities. Time integration is by the Houbolt method or central differences. The stiffeners may be due to concentrated or distributed eccentric rings and spring supports at arbitrary angles around the circumference of the elements. Check-out problems include the comparison of solutions from DYNAPLAS with experimental and other computer solutions for rings and conical and cylindrical shells. A hypothetical submarine including stiffeners and missile tube is studied under a combination of hydrostatic and dynamically applied asymmetrical pressure loadings.


1992 ◽  
Vol 58 (556) ◽  
pp. 2336-2344
Author(s):  
Hideomi OHTSUBO ◽  
Hideharu NAKAMURA ◽  
Shinichi MATSUURA ◽  
Kunio KOKUBO ◽  
Takashi OHTSUBO

1976 ◽  
Vol 8 (4) ◽  
pp. 483-486
Author(s):  
I. S. Chernyshenko ◽  
G. K. Sharshukov

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