NUMERICAL STUDY OF THE DEPENDENCE OF THE CRITICAL FLUTTER SPEED AND TIME OF A PLATE ON RHEOLOGICAL PARAMETERS

被引：5

作者：

Khudayarov, B. A. ^{[1
]}

机构：

[1] Tashkent Inst Irrigat & Ameliorat, Tashkent, Uzbekistan

来源：

INTERNATIONAL APPLIED MECHANICS | 2008年 / 44卷 / 06期

关键词：

flutter; viscoelastic plate; numerical algorithm; integro-differential equations; critical speed; critical time;

D O I：

10.1007/s10778-008-0078-2

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

The nonlinear flutter of some aircraft elements is modeled. A viscoelastic model is used. Numerical algorithms for solving integro-differential equations are developed. The critical flutter speed and time for a viscoelastic plate are determined

引用

页码：676 / 682

页数：7

共 13 条

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