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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通胀与轨迹特性研究

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A tandem compound parachute system composed of a rotating parachute and a round parachute is designed. Using fluid-structure interaction method, the inflation process of the parachute system is simulated. The canopy shape change, the time-historical curves of spinning rate and opening load are obtained. The tower test is conducted to verify the simulation results, and the effects of structure parameters on the system performance are analyzed. The trajectory characteristics of the tandem compound parachute-submunition system are simulated by RecurDyn. The results show that the tandem compound parachute system can inflate successfully with the condition of low flow velocity and come to rotate. The tandem compound parachute system can offer steady spinning rate and falling velocity for smart submunition. Decreasing the canopy area of the rotating parachute can increase the decelerating and spinning efficiency of the parachute system, but the canopy with too small area will make the parachute cords twisted.
机译:设计由旋转降落伞和圆形降落伞组成的串联复合降落伞系统。使用流体结构相互作用方法,模拟降落伞系统的膨胀过程。冠层形状改变,获得纺纱速率和开口负荷的时间历史曲线。进行塔式测试以验证仿真结果,分析了结构参数对系统性能的影响。串联复合降落伞 - 中置系统的轨迹特性由Recurdyn模拟。结果表明,串联复合降落伞系统可以成功地充气,流量速度低,旋转。串联复合降落伞系统可以为智能提交提供稳定的纺纱速率和下降速度。减小旋转降落伞的顶篷区域可以增加降落伞系统的减速和纺纱效率,但是面积太小的冠层会使降落伞扭曲。

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