Calculating distribution of parallel landing gear wheel load

被引:0
|
作者
Feng, Yunwen [1 ]
Kuang, Aimin [1 ]
Pan, Wenting [2 ]
Feng, Yuansheng [1 ]
机构
[1] College of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
[2] The First Aircraft Design and Research Institute, AVIC-I, Xi'an 710089, China
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:467 / 471
相关论文
共 50 条
  • [21] A method for determining the horizontal impact load based on the rotational speed of the aircraft's wheel in a landing gear drop test
    Wang, Huaitao
    Wu, Dafang
    Wang, Feng
    Ren, Haoyuan
    INTERNATIONAL JOURNAL OF CRASHWORTHINESS, 2018, 23 (06) : 627 - 634
  • [22] A New Method for Determining Horizontal Impact Load Based on Rotational Speed of Aircraft Wheel in Landing Gear Drop Test
    Wang Huaitao
    Wu Dafang
    Wang Feng
    2017 INTERNATIONAL CONFERENCE ON MECHANICAL, MATERIAL AND AEROSPACE ENGINEERING (2MAE 2017), 2017, 114
  • [23] Flow topology around a simplified two-wheel landing gear
    G. Feltham
    A. Ekmekci
    Journal of Visualization, 2014, 17 : 211 - 219
  • [24] Determining Wheel Forces and Moments on Aircraft Landing Gear with a Dynamometer Sensor
    Pytka, Jaroslaw
    Budzynski, Piotr
    Lyszczyk, Tomasz
    Jozwik, Jerzy
    Michalowska, Joanna
    Tofil, Arkadiusz
    Blazejczak, Dariusz
    Laskowski, Jan
    SENSORS, 2020, 20 (01)
  • [25] Flow topology around a simplified two-wheel landing gear
    Feltham, G.
    Ekmekci, A.
    JOURNAL OF VISUALIZATION, 2014, 17 (03) : 211 - 219
  • [26] Surface topology on the wheels of a generic four-wheel landing gear
    Lazos, B
    AIAA JOURNAL, 2002, 40 (12) : 2402 - 2411
  • [27] LOAD DISTRIBUTION ON GEAR TEETH
    GROMAN, MB
    RUSSIAN ENGINEERING JOURNAL-USSR, 1967, 47 (05): : 44 - &
  • [28] Analysis of Effects on the Load of Nose Landing Gear by Towbarless Traction
    Mu, Mengxin
    Liu, Hui
    Chen, Dawei
    PROCEEDINGS OF 2020 IEEE 2ND INTERNATIONAL CONFERENCE ON CIVIL AVIATION SAFETY AND INFORMATION TECHNOLOGY (ICCASIT), 2020, : 762 - 768
  • [29] Effect of impact load on threaded connection of an aircraft landing gear
    Miao, Hong
    Zuo, Dun-Wen
    Wang, Hong-Feng
    Wang, Hong-Jun
    Zhendong yu Chongji/Journal of Vibration and Shock, 2010, 29 (02): : 208 - 211
  • [30] Investigation of landing gear wheel shimmy taking into account damper frequency characteristics
    Metrikin V.S.
    Peisel M.A.
    Russian Aeronautics, 2009, 52 (02): : 240 - 244