Thermal modal test method for a wing structure considering aerodynamic heating

被引:0
|
作者
Liu, Hao [1 ]
Li, Xiao-Dong [1 ]
Yang, Wen-Qi [1 ]
Sun, Xia-Sheng [1 ]
机构
[1] College of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, China
来源
关键词
D O I
10.13465/j.cnki.jvs.2015.13.018
中图分类号
学科分类号
摘要
引用
收藏
页码:101 / 108
相关论文
共 50 条
  • [21] Solar Water Heating Thermal Performance Test using an Outdoor Test Method
    Hameer, Sameer
    van Niekerk, Johannes
    2021 IEEE PES/IAS POWERAFRICA CONFERENCE, 2021, : 299 - 302
  • [22] METHOD OF AERODYNAMIC DESIGNING OF WING PROFILE OF SCREEN PLANES
    ILINSKII, AN
    ILINSKII, NB
    MAKLAKOV, DV
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1995, (02): : 54 - 63
  • [24] USE OF LIQUID CRYSTALS IN AN AERODYNAMIC HEATING TEST.
    Ardasheva, M.M.
    Ryzhkova, M.V.
    Fluid Mechanics, Soviet Research, 1977, 6 (06): : 128 - 136
  • [25] Wing aerodynamic optimization method for aircraft family design
    Yong, Mingpei
    Yu, Xiongqing
    Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 2008, 40 (04): : 475 - 479
  • [26] METHOD FOR SIMULTANEOUS WING AERODYNAMIC AND STRUCTURAL LOAD PREDICTION
    DRELA, M
    AIAA 7TH APPLIED AERODYNAMICS CONFERENCE: A COLLECTION OF TECHNICAL PAPERS, 1989, : 322 - 332
  • [27] METHOD FOR SIMULTANEOUS WING AERODYNAMIC AND STRUCTURAL LOAD PREDICTION
    DRELA, M
    JOURNAL OF AIRCRAFT, 1990, 27 (08): : 692 - 699
  • [28] Modal analysis and extraction method for the frame structure considering soil-structure interaction effect
    Pan, Danguang
    Tan, Jinpeng
    Fu, Xiangqiu
    Huang, Ying
    Li, Xueju
    COMPUTERS AND GEOTECHNICS, 2023, 157
  • [29] Integrated Aerodynamic Thermal Structure Design Optimization Method of Lifting Surfaces
    Zhu, Huaguang
    Liu, Li
    Zhou, Sida
    Li, Yulin
    JOURNAL OF AIRCRAFT, 2012, 49 (05): : 1521 - 1526
  • [30] ENGINEERING AERODYNAMIC HEATING METHOD FOR HYPERSONIC FLOW
    RILEY, CJ
    DEJARNETTE, FR
    JOURNAL OF SPACECRAFT AND ROCKETS, 1992, 29 (03) : 327 - 334