Development of aeroelastic response solution sequence with DMAP language for freeplay nonlinear structure

被引:0
|
作者
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China [1 ]
机构
来源
Nanjing Hangkong Hangtian Daxue Xuebao | 2007年 / 1卷 / 41-46期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:41 / 46
相关论文
共 2 条
  • [1] Nonlinear aeroelastic response of a typical airfoil section with control surface freeplay
    Tang, DM
    Kholodar, D
    Dowell, EH
    COLLECTION OF THE 41ST AIAA/ASME/ASCE/AHS/ASC STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE AND EXHIBIT, VOL 1 PTS 1-3, 2000, : 1514 - 1523
  • [2] Nonlinear aeroelastic response analysis of rotor blade modeled as composite thin-walled structure
    Mechanical and Electronical Institute, Shandong University of Science and Technology, Qingdao 266590, China
    Taiyangneng Xuebao, 1 (105-112):