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Simulation Research in Measurement of Opening Overload of Life-saving Parachute in Dummy High-speed Airdrop

机译:虚拟高速AIRDROP中救生降落伞开口过载测量的仿真研究

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In this paper, CFD and ADAMS virtual prototyping technology were used to simulate the whole airdrop process. Three cases with different hanging positions and hanging postures were simulated. We divided the whole airdrop process into four stages, leaving cabin stage, pull-out stage, opening stage and stable landing stage. Firstly, the complex aerodynamic characteristics of trunk dummy were calculated by CFD method. Before pull-out parachute, leaving cabin stage, the varying attitude of dummy was simulated by dynamic mesh method using CFD software. Secondly, the pull-out stage and opening stage model were set up in ADAMS. In pull-out stage, parachute was discrete into damping spring and mess particle connection model. The opening stage and stable landing stage was also simulated in ADAMS. Aerodynamic drag characteristic and additional quality were deal with empirical method. Lastly, the simulate results were compared with experimental results and then analyzed on phase plane. These simulation results match experimental results well in temporal domain. There two peaks in overload data, one is pull-out peak, and another is opening peak. They have a negative correlation, which also meet the test results well. Phase plane was established by dummy angular and angular velocity. On phase plane, the state of dummy motion exhibit significant differences in leaving cabin stage, pull-out stage and opening stage. On phase plane, the opening shocks of dummy were smaller, which could be considered as favorable parachute opening area. It shows that there is a strong dependence between the dummy attitude, angular velocity and the overload of dummy center at the parachute opening moment. However, the dummy hanging position and hanging posture in cabin almost have no effect on overload data. In summary, the model of this paper can simulate all the airdrop process. Using this simulation method, we reproduce the problem in life-saving parachute and dummy system airdrop, and analyzed the issue. We found a good regularity on phase plane, which show us a favorable dummy attitude when parachute is opening.
机译:在本文中,CFD和ADAMS虚拟原型设计技术用于模拟整个AICLOP过程。模拟了不同悬挂位置和悬挂姿势的三个案例。我们将整个AirDrop过程划分为四个阶段,离开舱室级,拉出阶段,开口阶段和稳定的着陆阶段。首先,通过CFD方法计算树干虚拟的复杂空气动力学特性。在拉伸降落伞之前,通过使用CFD软件通过动态网格方法模拟托盘阶段的变化姿态。其次,在亚当斯中建立了拉出阶段和开放阶段模型。在拉出阶段,降落伞是离散的阻尼弹簧和混乱粒子连接模型。在Adams中也模拟了开口阶段和稳定的着陆阶段。空气动力学阻力特征和额外的质量是以经验的方式应对。最后,将模拟结果与实验结果进行比较,然后在相面上分析。这些仿真结果匹配时间域中的实验结果。过载数据中有两个峰值,一个是拉出峰值,另一个是开口峰值。它们具有负相关性,这也很好地满足了测试结果。通过虚拟角度和角速度建立相平面。在相平面上,伪动状态表现出留下舱室阶段,拉出阶段和开口阶段的显着差异。在相平面上,假人的开口冲击较小,这可以被认为是有利的降落伞开口区域。它表明,在降落伞开放时刻,虚拟姿态,角速度和虚拟中心的过载有很强的依赖。然而,舱室中的伪悬挂位置和悬挂姿势几乎对过载数据没有影响。总之,本文的模型可以模拟所有AICDOP过程。使用这种仿真方法,我们重现了节省救生降落伞和虚拟系统AITDOP的问题,并分析了这个问题。我们在阶段飞机上发现了一个很好的规律性,当降落伞打开时,它向我们展示了一个有利的假姿态。

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