| タイトル | Finite-element nonlinear transient response computer programs PLATE 1 and CIVM-PLATE 1 for the analysis of panels subjected to impulse or impact loads |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810017954 |
| 著者（英） | French, S. E.; Rodal, J. J. A.; Spilker, R. L.; Witmer, E. A. |
| 著者所属（英） | Massachusetts Inst. of Tech. |
| 発行日 | 1980-09-01 |
| 言語 | eng |
| 内容記述 | Two computer programs are described for predicting the transient large deflection elastic viscoplastic responses of thin single layer, initially flat unstiffened or integrally stiffened, Kirchhoff-Lov ductile metal panels. The PLATE 1 program pertains to structural responses produced by prescribed externally applied transient loading or prescribed initial velocity distributions. The collision imparted velocity method PLATE 1 program concerns structural responses produced by impact of an idealized nondeformable fragment. Finite elements are used to represent the structure in both programs. Strain hardening and strain rate effects of initially isotropic material are considered. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 81N26491
ASRL-TR-154-14
NASA-CR-165215 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/168727 |
