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飞翼布局阻力类偏航操纵装置操纵特性分析

李忠剑 马东立

李忠剑, 马东立. 飞翼布局阻力类偏航操纵装置操纵特性分析[J]. 北京航空航天大学学报, 2014, 40(5): 695-700. doi: 10.13700/j.bh.1001-5965.2013.0340
引用本文: 李忠剑, 马东立. 飞翼布局阻力类偏航操纵装置操纵特性分析[J]. 北京航空航天大学学报, 2014, 40(5): 695-700. doi: 10.13700/j.bh.1001-5965.2013.0340
Li Zhongjian, Ma Dongli. Control characteristics analysis of drag yawing control devices of flying wing configuration[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(5): 695-700. doi: 10.13700/j.bh.1001-5965.2013.0340(in Chinese)
Citation: Li Zhongjian, Ma Dongli. Control characteristics analysis of drag yawing control devices of flying wing configuration[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(5): 695-700. doi: 10.13700/j.bh.1001-5965.2013.0340(in Chinese)

飞翼布局阻力类偏航操纵装置操纵特性分析

doi: 10.13700/j.bh.1001-5965.2013.0340
详细信息
    作者简介:

    李忠剑(1988- ),男,福建龙岩人,硕士生,xyzj201314@sina.com.

  • 中图分类号: V221

Control characteristics analysis of drag yawing control devices of flying wing configuration

  • 摘要: 飞翼布局取消了常规的垂尾和方向舵,存在较严重的航向操纵与控制问题,需要重点掌握偏航操纵舵面的配置特点与操纵特性.针对飞翼布局最常采用的两种阻力类偏航操纵装置:开裂式方向舵和嵌入面,介绍了研究现状、受力特点,利用数值仿真方法,详细分析了偏航操纵特性、三轴操纵耦合特性以及对气动特性和稳定特性的影响规律,对比了这两种舵面在操纵特性方面的共同点和差异性,并揭示了内在的影响机理.可为解决飞翼布局偏航操纵问题以及阻力类偏航操纵装置的工程化应用提供基础.

     

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出版历程
  • 收稿日期:  2013-06-19
  • 刊出日期:  2014-05-20

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