Flutter prediction of composite wing using finite element method with equivalent stiffness

被引：0
|
作者：
Ouyang, Xing [1 ]
Yu, Xiong-Qing [1 ]
Wang, Yu [1 ]
机构：
[1] Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
来源：
Zhendong Gongcheng Xuebao/Journal of Vibration Engineering | 2015年 / 28卷 / 03期
关键词：
Aircraft preliminary design - Equivalent stiffness - Flutter analysis - Model and analysis - Preliminary design - Stiffness matrices - Stringer-stiffened panels - Structural layout;
D O I：
10.16385/j.cnki.issn.1004-4523.2015.03.009
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：404 / 410
相关论文
共 50 条
  • [31] FLUTTER ANALYSIS OF THIN CRACKED PANELS USING THE FINITE-ELEMENT METHOD
    CHEN, WH
    LIN, HC
    AIAA JOURNAL, 1985, 23 (05) : 795 - 801
  • [32] Active and passive suppressions of nonlinear panel flutter using finite element method
    Moon, SH
    Kim, SJ
    AIAA JOURNAL, 2001, 39 (11) : 2042 - 2050
  • [33] Prediction of crack path in concrete-like composite using extended finite element method
    Gontarz, Jakub
    Podgorski, Jerzy
    ADVANCES IN SCIENCE AND TECHNOLOGY-RESEARCH JOURNAL, 2025, 19 (02) : 239 - 254
  • [34] FINITE-ELEMENT FLUTTER ANALYSIS OF LAMINATED COMPOSITE PANELS
    CHOWDARY, TVR
    PARTHAN, S
    SINHA, PK
    COMPUTERS & STRUCTURES, 1994, 53 (02) : 245 - 251
  • [35] Prediction of soil stresses using the finite element method
    Raper, R.L.
    Erbach, D.C.
    Transactions of the American Society of Agricultural Engineers, 1990, 33 (03): : 725 - 730
  • [36] Beat Control Method Using the Finite Element Analysis of an Equivalent Ring
    Kim, Seockhyun
    Cui, Chengxun
    JOURNAL OF THE ACOUSTICAL SOCIETY OF KOREA, 2008, 27 (07): : 365 - 371
  • [37] Coupling using equivalent generalized quantities :: A finite element method approach
    Piña, SEF
    PROCEEDINGS OF ISMA 2002: INTERNATIONAL CONFERENCE ON NOISE AND VIBRATION ENGINEERING, VOLS 1-5, 2002, : 1757 - 1761
  • [38] NONLINEAR PANEL FLUTTER BY FINITE-ELEMENT METHOD
    SARMA, BS
    VARADAN, TK
    AIAA JOURNAL, 1988, 26 (05) : 566 - 574
  • [39] Shape monitoring of morphing wing structures using the inverse Finite Element Method
    Biscotti, Vincenzo
    Roy, Rinto
    Gherlone, Marco
    COMPUTERS & STRUCTURES, 2025, 309
  • [40] Determination of the Wing Conveyor Idlers' Axial Loads Using the Finite Element Method
    Miskovic, Zarko
    Mitrovic, Radivoje
    Tasic, Milan
    Tasic, Marko
    Danko, Jan
    EXPERIMENTAL AND NUMERICAL INVESTIGATIONS IN MATERIALS SCIENCE AND ENGINEERING, 2019, 54 : 174 - 192
12345