Spacecraft Recovery & Remote Sensing, Volume. 45, Issue 2, 29(2024)

Research on Load Outbound by the Method of Dynamic Nesting Grid

Chaoqun CHEN... Hongying ZHANG*, Jianping CHEN, Mingbo TONG and Jianjiang ZENG |Show fewer author(s)
Author Affiliations
  • College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • show less
    Figures & Tables(11)
    [in Chinese]
    [in Chinese]
    [in Chinese]
    [in Chinese]
    [in Chinese]
    [in Chinese]
    [in Chinese]
    [in Chinese]
    [in Chinese]
    • Table 1. NACA64A010 airfoil dimensions

      View table
      View in Article

      Table 1. NACA64A010 airfoil dimensions

      计算参数数值
      前缘后掠角/(°)45
      后缘后掠角/(°)0
      翼根弦长/mm7 620
      挂架2 200 mm×150 mm×610 mm
    • Table 2. NACA0008 tail airfoil missile dimensions

      View table
      View in Article

      Table 2. NACA0008 tail airfoil missile dimensions

      计算参数数值计算参数数值
      质量/kg907前缘弹射力位置/mm1 237.5(相对于导弹头部)
      长度/mm3 017.5前缘弹射力大小/kN10.7
      直径/mm500后缘弹射力大小/kN42.7
      质心/mm1 417(原点在导弹头部)后缘弹射力位置/mm1 746.5(相对于导弹头部)
      转动惯量/kg·m227作用距离/mm100
      转动惯量/kg·m2488作用时间/s0.054
    Tools

    Get Citation

    Copy Citation Text

    Chaoqun CHEN, Hongying ZHANG, Jianping CHEN, Mingbo TONG, Jianjiang ZENG. Research on Load Outbound by the Method of Dynamic Nesting Grid[J]. Spacecraft Recovery & Remote Sensing, 2024, 45(2): 29

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category:

    Received: Aug. 16, 2023

    Accepted: --

    Published Online: May. 29, 2024

    The Author Email: ZHANG Hongying (zhanghy@nuaa.edu.cn)

    DOI:10.3969/j.issn.1009-8518.2024.02.003

    Topics