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Flow Characteristics of Double-Cruciform Parachute at Inflating and Inflated Conditions

机译:充气和充气条件下双十字形降落伞的流动特性

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摘要

The fluid-structure interaction (FSI) between the canopy and flow field on the inflating and inflated conditions is investigated based on the arbitrary Lagrange-Euler (ALE) method, in both a single-and double-cruciform parachute systems.The projection area of canopy is calculated in the inflation process.The flow field characteristics and the interaction between canopies are analyzed.Results showed that, with free stream velocity of 50m/s, overinflation phenomenon would not occur during the inflation process of the double-cruciform-parachute system, because the collision and extrusion of the two canopies during inflation obstructed the oscillation of the inner gores.Concurrently, compared with the single-cruciform parachute, the vortex motion in the wake of double-cruciform-parachute is more intense.Thus the double-cruciform parachute system oscillated at a velocity of 50 m/s with an angle of less than 6.8°.By comparison, the oscillation angle of the single-cruciform parachute was within3.5°at the velocity of 50m/s.The results are consistent with those of the wind tunnel test.
机译:在单和双十字形降落伞系统中,基于任意拉格朗日-欧拉(ALE)方法,研究了充气和充气条件下机盖与流场之间的流固耦合(FSI)。结果表明,在自由流速度为50m / s的情况下,双十字形降落伞系统在充气过程中不会发生过充气现象。由于在膨胀过程中两个顶篷的碰撞和挤压阻碍了内孔的振荡。因此,与单十字形降落伞相比,双十字形降落伞后的涡旋运动更加强烈。十字形降落伞系统以50 m / s的速度振荡,且角度小于6.8°。相比之下,单十字形降落伞的振荡角为在3.5°,50m / s的速度下进行。结果与风洞试验的结果一致。

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  • 来源
    《南京航空航天大学学报(英文版)》 |2018年第6期|992-999|共8页
  • 作者单位

    Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

    Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 计算空气动力学;
  • 关键词

  • 入库时间 2022-08-19 04:26:04
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