ANALYSIS OF THIN-WALL AIRCRAFT STRUCTURES IN THE GEOMETRICALLY NONLINEAR FORMULATION.

被引：0

作者：

Pavlov, V.A.

Safonov, A.S.

机构：

来源：

Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika) | 1983年 / 26卷 / 04期

关键词：

STRESSES; -; Analysis;

D O I：

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摘要：

Based on Odinokov's theory we construct a slightly-tapered reinforced structure analysis technique that makes it possible to determine the stress-strain state with account for the influence of displacement of the structure axis. Nonlinear intergrodifferential equations are obtained.

引用

页码：45 / 49