INCREMENTAL HARMONIC BALANCE METHOD FOR AIRFOIL FLUTTER WITH MULTIPLE STRONG NONLINEARITIES

doi:10.1007/s10483-006-0711-y

Applied Mathematics and Mechanics (English Edition) ›› 2006, Vol. 27 ›› Issue (7): 953-958 .doi: https://doi.org/10.1007/s10483-006-0711-y

INCREMENTAL HARMONIC BALANCE METHOD FOR AIRFOIL FLUTTER WITH MULTIPLE STRONG NONLINEARITIES

蔡铭, 刘济科, 李军

收稿日期:2004-10-10 修回日期:2006-03-21 出版日期:2006-07-18 发布日期:2006-07-18
通讯作者: 刘济科

INCREMENTAL HARMONIC BALANCE METHOD FOR AIRFOIL FLUTTER WITH MULTIPLE STRONG NONLINEARITIES

CAI Ming, LIU Ji-ke, LI Jun

1. School of Engineering, Sun Yat-sen University, Guangzhou 510275, P. R. China;
2. Deptartment of Applied Mechanics and Engineering, Sun Yat-sen University, Guangzhou 510275, P. R. China

Received:2004-10-10 Revised:2006-03-21 Online:2006-07-18 Published:2006-07-18
Contact: LIU Ji-ke

摘要/Abstract

中图分类号:

蔡铭;刘济科;李军. INCREMENTAL HARMONIC BALANCE METHOD FOR AIRFOIL FLUTTER WITH MULTIPLE STRONG NONLINEARITIES[J]. Applied Mathematics and Mechanics (English Edition), 2006, 27(7): 953-958 .

CAI Ming;LIU Ji-ke;LI Jun. INCREMENTAL HARMONIC BALANCE METHOD FOR AIRFOIL FLUTTER WITH MULTIPLE STRONG NONLINEARITIES[J]. Applied Mathematics and Mechanics (English Edition), 2006, 27(7): 953-958 .

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INCREMENTAL HARMONIC BALANCE METHOD FOR AIRFOIL FLUTTER WITH MULTIPLE STRONG NONLINEARITIES

INCREMENTAL HARMONIC BALANCE METHOD FOR AIRFOIL FLUTTER WITH MULTIPLE STRONG NONLINEARITIES

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