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Titlebook: Computational Mechanics of Nonlinear Response of Shells; Wilfried B. Kr?tzig,Eugenio O?ate Book 1990 Springer-Verlag Berlin Heidelberg 199

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發(fā)表于 2025-3-23 10:46:00 | 只看該作者
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發(fā)表于 2025-3-23 16:32:18 | 只看該作者
An Assumed Strain Mixed Formulation for Nonlinear Shellsgenerate solid shell element concept and the Hellinger-Reissner principle with independent strain field. The independent strain field is divided into a lower order part and a higher order part. Using the equivalence between displacement formulation and mixed formulation, the lower order part is repl
13#
發(fā)表于 2025-3-23 21:24:56 | 只看該作者
Refined Finite Element Laminated Models for the Static and Dynamic Elasto-Plastic Analysis of Anisotnted. A layered approach is adopted for solution with displacement variables assumed at each laminate interface. Elastic-plastic numerical analysis is performed based on flow theory and a Huber-Mises yielding surface extended by Hill for fully three dimensional anisotropic materials. Dynamic analysi
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發(fā)表于 2025-3-23 23:07:52 | 只看該作者
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發(fā)表于 2025-3-24 03:22:17 | 只看該作者
Nonlinear Shell Analysis of the Space Shuttle Solid Rocket Boostersnding of the failure which destroyed the Space Shuttle Challenger. This paper describes nonlinear shell analyses that were performed to characterize the behavior of an overall SRB structure and a segment of the SRB in the vicinity of the External Tank Attachment (ETA) ring. Shell finite element mode
16#
發(fā)表于 2025-3-24 09:06:13 | 只看該作者
17#
發(fā)表于 2025-3-24 11:57:46 | 只看該作者
Dynamic Stability Analysis of Shell Structureserion is shown. The procedure can be extended to the eigenproblem for the load parameter in order to approximate the critical step load to some extent directly. Numerical examples demonstrate the quality of the proposed method.
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發(fā)表于 2025-3-24 15:17:52 | 只看該作者
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