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1190 SATYANAD~M ATLURI<br />

91s<br />

2. 4c0<br />

z<br />

la<br />

200<br />

- Exact soluti<strong>on</strong> <strong>for</strong> c,=O<br />

A Ref. 18, A$=300. predictor<br />

corrector method<br />

0 Present soiutl<strong>on</strong>. A6830<br />

FIG. 3<br />

CONCLUSIONS<br />

A c<strong>on</strong>sistent variati<strong>on</strong>al <strong>for</strong>mulati<strong>on</strong> <strong>of</strong> <strong>the</strong> <strong>hybrid</strong> <strong>stress</strong> <strong>finite</strong> <strong>element</strong> <strong>model</strong> <strong>for</strong><br />

<strong>analysis</strong> <strong>of</strong> large deflecti<strong>on</strong> problems, in c<strong>on</strong>juncti<strong>on</strong> with an <strong>incremental</strong> approach, is<br />

presented. The c<strong>on</strong>cept <strong>of</strong> initial <strong>stress</strong>es is imployed. In each <strong>incremental</strong> step, <strong>the</strong> assumed<br />

<strong>incremental</strong> Piola-Kirch<strong>of</strong>f <strong>stress</strong>es satisfy <strong>the</strong> linearized <strong>incremental</strong> equilibrium equati<strong>on</strong>s<br />

in <strong>the</strong> interior <strong>of</strong> each <strong>finite</strong> <strong>element</strong>; whereas, a compatible <strong>incremental</strong> displacement<br />

field is assumed at <strong>the</strong> boundary <strong>of</strong> each <strong>element</strong>. A check <strong>on</strong> <strong>the</strong> equilibrium <strong>of</strong><br />

initial <strong>stress</strong>es in <strong>the</strong> current reference geometry, be<strong>for</strong>e <strong>the</strong> additi<strong>on</strong> <strong>of</strong> a fur<strong>the</strong>r loadincrement,<br />

is included to improve <strong>the</strong> numerical accuracy. The method leads to an <strong>incremental</strong><br />

stiffness matrix and is easily adaptable to existing computer programs,using <strong>the</strong><br />

stiffness approach.<br />

Since <strong>the</strong> <strong>hybrid</strong> <strong>stress</strong> <strong>model</strong> has proven to be a valuable tool in <strong>the</strong> linear <strong>analysis</strong><br />

<strong>of</strong> complex problems such as sandwich plates and shells, and problems with singularities<br />

[Refs. 14 and 111, it can be expected to be <strong>of</strong> equal value in large deflecti<strong>on</strong> problems.<br />

Present results <strong>for</strong> <strong>the</strong> large deflecti<strong>on</strong>s <strong>of</strong> a shallow beam show good agreement with<br />

existing results using displacement <strong>model</strong>s. Fur<strong>the</strong>r results <strong>on</strong> <strong>the</strong> applicati<strong>on</strong> <strong>of</strong> <strong>the</strong><br />

present method to <strong>the</strong> <strong>analysis</strong> <strong>of</strong> a toroidal shell will be presented later.<br />

Acknowledgements-The author wishes to thank Pr<strong>of</strong>essor T. H. H. Pian <strong>of</strong> MIT. and Pr<strong>of</strong>essor K. Washizu<br />

<strong>of</strong> <strong>the</strong> University <strong>of</strong> Tokyo <strong>for</strong> many helpful comments and suggesti<strong>on</strong>s.<br />

REFERENCES<br />

[I] T. H. H. PUN and P. TONG, Basis <strong>of</strong> <strong>finite</strong> <strong>element</strong> method <strong>for</strong> solid c<strong>on</strong>tinua. Inf. J. Numerical Methods<br />

Engng 1 (l), 3-28 (1969).<br />

[2] S. ATLURI and T. H. H. PIAN, Theoretical <strong>for</strong>mulati<strong>on</strong> <strong>of</strong> <strong>finite</strong> <strong>element</strong> methods in <strong>the</strong> linear-elastic <strong>analysis</strong><br />

<strong>of</strong> general shells. J. Struct. Mech. 1 (I), l-43 (1972).<br />

[3] J. T. ODEN, Finite Elements <strong>of</strong>N<strong>on</strong>linear C<strong>on</strong>tinua. McGraw-Hill (1971).<br />

[4] T. H. H. PUN, Derivati<strong>on</strong> <strong>of</strong> <strong>element</strong> stiffness matrices by assumed <strong>stress</strong> distributi<strong>on</strong>s. AIAA J. 2 (7),<br />

1333-1336 (1964).

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