Flutter of delta wing under aerodynamic heating

被引:0
|
作者
Ye, Xianhui [1 ]
Yang, Yiren [1 ]
机构
[1] Dept. of Appl. Mechanics and Eng., Southwest Jiaotong University, Chengdu 610031, China
关键词
D O I
暂无
中图分类号
学科分类号
摘要
10
引用
收藏
页码:62 / 66
相关论文
共 50 条
  • [31] AERODYNAMIC EFFECTS OF DELTA PLANFORM TIP SAILS ON WING PERFORMANCE
    TRAUB, LW
    JOURNAL OF AIRCRAFT, 1994, 31 (05): : 1156 - 1159
  • [32] Aerodynamic effects of delta planform tip sails on wing performance
    Traub, Lance W., 1600, AIAA, Washington, DC, United States (31):
  • [33] Effects of Unsteady Freestream on Aerodynamic Characteristics of Pitching Delta Wing
    Shi, Zhi-Wei
    Ming, Xiao
    JOURNAL OF AIRCRAFT, 2008, 45 (06): : 2182 - 2185
  • [34] Effects of unsteady freestream on aerodynamic characteristics of pitching delta wing
    Shi, Zhi-Wei
    Ming, Xiao
    Journal of Aircraft, 1600, 45 (06): : 2182 - 2185
  • [35] AEROTHERMOELASTIC MODEL OF PANEL FLUTTER WITH CONSIDERATION OF THE HISTORY EFFECTS OF AERODYNAMIC HEATING
    Li, Kailun
    Zhang, Jiazhong
    Mei, Guanhua
    INTERNATIONAL JOURNAL OF APPLIED MECHANICS, 2012, 4 (03)
  • [36] Aerodynamic performance of a wing with a deflected tip-mounted reverse half-delta wing
    T. Lee
    Y. Y. Su
    Experiments in Fluids, 2012, 53 : 1221 - 1232
  • [37] Aerodynamic performance of a wing with a deflected tip-mounted reverse half-delta wing
    Lee, T.
    Su, Y. Y.
    EXPERIMENTS IN FLUIDS, 2012, 53 (05) : 1221 - 1232
  • [38] Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations
    LeeRausch, EM
    Batina, JT
    JOURNAL OF AIRCRAFT, 1996, 33 (06): : 1139 - 1147
  • [39] CALCULATED EFFECT OF FREESTREAM TURBULENCE ON AERODYNAMIC CHARACTERISTICS OF A DELTA-WING
    POLLAK, J
    LAN, CE
    AIAA JOURNAL, 1995, 33 (09) : 1734 - 1736
  • [40] Investigation of aerodynamic characteristics on an oscillating delta wing in low-speed
    Hong, Jinsen
    Fu, Guangming
    Wang, Qiang
    Qidong Shiyan yu Celiang Kongzhi/Aerodynamic Experiment and Measurement & Control, 12 (01): : 38 - 43