Lessons from application of equivalent plate structural modeling to an HSCT wing

被引:0
|
作者
机构
[1] Livne, Eli
[2] Sels, Robert A.
[3] Bhatia, Kumar G.
来源
Livne, Eli | 1600年 / AIAA, Washington, DC, United States卷 / 31期
关键词
Wings;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [31] Structural dynamics of a cantilever wing-like anisotropic swept plate
    Santini, P
    Gasbarri, P
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2000, 19 (14) : 1112 - 1146
  • [32] Lessons learned from a trial application of requirements modeling using statecharts
    Nobe, CR
    Warner, WE
    PROCEEDINGS OF THE SECOND INTERNATIONAL CONFERENCE ON REQUIREMENTS ENGINEERING, 1996, : 86 - 93
  • [33] Application of Equivalent Air Gap Method in Uniaxial Crystal Plate
    Ren Wen-Yi
    Zhang Chun-Min
    Mu Ting-Kui
    CHINESE PHYSICS LETTERS, 2009, 26 (08)
  • [34] FURTHER GENERALIZATION OF AN EQUIVALENT PLATE REPRESENTATION FOR AIRCRAFT STRUCTURAL-ANALYSIS
    GILES, GL
    JOURNAL OF AIRCRAFT, 1989, 26 (01): : 67 - 74
  • [35] Neural network modeling of structured packing height equivalent to a theoretical plate
    Pollock, GS
    Eldridge, RB
    INDUSTRIAL & ENGINEERING CHEMISTRY RESEARCH, 2000, 39 (05) : 1520 - 1525
  • [36] Structural-Optimization Strategy for Composite Wing Based on Equivalent Finite Element Model
    Wang, Yu
    Ouyang, Xing
    Yin, Hailian
    Yu, Xiongqing
    JOURNAL OF AIRCRAFT, 2016, 53 (02): : 351 - 359
  • [37] Analysis and flexible structural modeling for oscillating wing utilizing aeroelasticity
    Shao, Ke
    Wu, Zhigang
    Yang, Chao
    1600, Chinese Journal of Aeronautics (21):
  • [38] Rapid wing structural finite element modeling and automated adjustment
    Luo, Mingqiang
    Feng, Haocheng
    Liu, Hu
    Wu, Zhe
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2011, 37 (06): : 680 - 684
  • [39] Analysis and Flexible Structural Modeling for Oscillating Wing Utilizing Aeroelasticity
    Shao Ke
    Wu Zhigang
    Yang Chao
    CHINESE JOURNAL OF AERONAUTICS, 2008, 21 (05) : 402 - 410
  • [40] Fast structural dynamic modeling and analysis for horizontally folding wing
    Ni, Yingge
    Zhang, Wei
    Lv, Yi
    REVISTA INTERNACIONAL DE METODOS NUMERICOS PARA CALCULO Y DISENO EN INGENIERIA, 2021, 37 (03):