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无人机投放分离特性仿真与优化 被引量:1

Simulation and Optimization of the Separation Process for UAV
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摘要 用于远程投放作战的无人机在与母机分离的过程中,其姿态变化与运动轨迹直接影响母机的安全性和自身稳定性。基于重叠网格技术,提出了一种流体-刚体运动耦合数值模拟方法,对无人机动态投放分离过程进行仿真。采用WPFS标模进行计算,发现仿真与试验结果吻合度高,数值模拟方法得到有效验证。采用上述数值模拟方法实现无人机投放过程的仿真,得到无人机在投放分离过程中位置与姿态随时间的变化规律。进一步基于仿真结果,完成了无人机弹射方案的优化设计。 In the separation process of long-range-launched UAV,the attitude change and trajectory directly affect the safety and stability of the parent aircraft.In this paper,based on overset grids,a fluid and rigid body motion coupling method was proposed to simulate the dynamic separation process of UAV.WPFS standard model was used for validation.It is found that the simulation results are in good agreement with the experimental data,and the numerical simulation method is effectively verified.The simulation of UAV separation process was realized by using the proposed numerical simulation method,and the change of UAV′s position and attitude with time in the process of separation was obtained.Based on the simulation results,an optimal design of UAV launching scheme was proposed.
作者 曾丽芳 黎军 王天琪 邵雪明 ZENG Li-fang;LI Jun;WANG Tian-qi;SHAO Xue-ming(School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027,China)
出处 《气体物理》 2022年第4期19-27,共9页 Physics of Gases
基金 浙江省重点研发计划(2020C05001)。
关键词 投放分离 数值模拟 重叠网格 无人机 稳定性 separation process numerical simulation overset grids UAV stability
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  • 1[1]GARCON F, TARAVEL P H, RAFFIN J C. Recent developments in captive trajectory systems of the ONERA Modane wind tunnel [R]. AIAA 2001-0579,2001.
  • 2Pearce D G, Stanley S A, Martin F W, Jr. Development of a large scale chimera grid system for the space shuttle launch vehicle[R]. AIAA-1993- 533, 1993.
  • 3Rogers S E, Cao H V, Su T Y. Grid generation for complex high-lift configurations[R]. AIAA-1998-3011, 1998.
  • 4Murman S M, Rizk Y M, Schiff L B. Coupled numerical simulation of the external and engine inlet flows for the F- 18 atlarge incidence[J]. Aircraft Design, 2000, 3(2): 65- 77.
  • 5Benek J A, Buning P G, Steger J L. A 3-D chimera grid embedding technique[R]. A1AA-1985 1523, 1985.
  • 6Meaking R L. A new method for establishing intergrid communication among systems of overset grids [R]. AIAA-1991 -1586, 1991.
  • 7Nakahashi K, Togashi F, Sharov D. Intergrid-boundary definition method for overset unstructured grid approach [J]. AIAA Journal, 2000, 38(11): 2077-2084.
  • 8Wey T C. Development of a mesh interface generator for overlapped structured grids[R]. AIAA 1994- 1924, 1994.
  • 9Cho K W, Kwon J H. Development of a fully systemized chimera methodology for steady/unsteady prohlems[J]. Journal of Aircraft, 1999, 36(6): 973- 980.
  • 10Noack R W. Resolution appropriate overset grid assembly for structured and unstructured grids [R]. AIAA 2003 4123, 2003.

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