• Spacecraft Recovery & Remote Sensing
  • Vol. 45, Issue 2, 29 (2024)
Chaoqun CHEN, Hongying ZHANG*, Jianping CHEN, Mingbo TONG, and Jianjiang ZENG
Author Affiliations
  • College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
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    DOI: 10.3969/j.issn.1009-8518.2024.02.003 Cite this Article
    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 Copy Citation Text show less
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    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 1. NACA64A010 airfoil 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
    Table 2. NACA0008 tail airfoil missile dimensions
    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
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