Effect of nonlinear terms in piston theory on characteristics of panel flutter

被引：0

作者：

Luo, Yuxiao ^{[1
]}

Ye, Kun ^{[1
]}

Ye, Zhengyin ^{[1
]}

机构：

[1] School of Aeronautics, Northwestern Polytechnical University, Xi′an,710072, China

来源：

Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University | / 42卷 / 04期

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Convergence of numerical methods - Flutter (aerodynamics) - Nonlinear analysis - Nonlinear equations - Number theory - Pistons - Supersonic aerodynamics - Supersonic aircraft - Supersonic flow

引用

页码：577 / 587

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