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

被引：0
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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;
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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.
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页码：45 / 49
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