| タイトル | On the Application of the Energy Method to Stability Problems |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050019403 |
| 著者（英） | Marguerre, Karl |
| 著者所属（英） | National Advisory Committee for Aeronautics |
| 発行日 | 1947-10-01 |
| 言語 | eng |
| 内容記述 | Since stability problems have come into the field of vision of engineers, energy methods have proved to be one of the most powerful aids in mastering them. For finding the especially interesting critical loads special procedures have evolved that depart somewhat from those customary in the usual elasticity theory. A clarification of the connections seemed desirable,especially with regard to the post-critical region, for the treatment of which these special methods are not suited as they are. The present investigation discusses this question-complex (made important by shell construction in aircraft) especially in the classical example of the Euler strut, because in this case - since the basic features are not hidden by difficulties of a mathematical nature - the problem is especially clear. The present treatment differs from that appearing in the Z.f.a.M.M. (1938) under the title "Uber die Behandlung von Stabilittatsproblemen mit Hilfe der energetischen Methode" in that, in order to work out the basic ideas still more clearly,it dispenses with the investigation of behavior at large deflections and of the elastic foundation;in its place the present version gives an elaboration of the 6th section and (in its 7 th and 8th secs.)a new example that shows the applicability of the general criterion to a stability problem that differs from that of Euler in many respects. |
| NASA分類 | Numerical Analysis |
| レポートNO | NACA-TM-1138 |
| 権利 | No Copyright |
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