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THE RESEARCH ON THE INFLATION AND TRAJECTORY CHARACTERISTICS OF TANDEM COMPOUND PARACHUTE SYSTEM

机译:串联复合降落伞系统的膨胀和弹道特性研究。

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A tandem compound parachute system composed of a rotating parachute and around parachute is designed. Using fluid-structure interaction method, the inflationprocess of the parachute system is simulated. The canopy shape change, thetime-historical curves of spinning rate and opening load are obtained. The tower testis conducted to verify the simulation results, and the effects of structure parameterson the system performance are analyzed. The trajectory characteristics of the tandemcompound parachute-submunition system are simulated by RecurDyn. The resultsshow that the tandem compound parachute system can inflate successfully with thecondition of low flow velocity and come to rotate. The tandem compound parachutesystem can offer steady spinning rate and falling velocity for smart submunition.Decreasing the canopy area of the rotating parachute can increase the deceleratingand spinning efficiency of the parachute system, but the canopy with too small areawill make the parachute cords twisted.
机译:由旋转降落伞和降落伞组成的串联复合降落伞系统。 设计圆形降落伞。采用流固耦合方法,膨胀 模拟了降落伞系统的运行过程。顶篷形状变化, 得到了纺丝速度和开松负荷的时间-历史曲线。塔测试 进行验证仿真结果以及结构参数的影响 对系统性能进行了分析。串联的轨迹特性 复合降落伞-子弹药系统由RecurDyn模拟。结果 表明串联复合降落伞系统可以成功地膨胀。 在低流速条件下旋转。串联复合降落伞 该系统可以为智能子弹药提供稳定的旋转速度和下降速度。 减小旋转降落伞的顶篷面积可以增加减速 和降落伞系统的旋转效率,但顶篷面积过小 会使降落伞绳扭曲。

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