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利于减少配平损失的太阳能飞机构型设计

阙建锋 王维军 吴宇

阙建锋, 王维军, 吴宇等 . 利于减少配平损失的太阳能飞机构型设计[J]. 北京航空航天大学学报, 2016, 42(7): 1479-1485. doi: 10.13700/j.bh.1001-5965.2015.0464
引用本文: 阙建锋, 王维军, 吴宇等 . 利于减少配平损失的太阳能飞机构型设计[J]. 北京航空航天大学学报, 2016, 42(7): 1479-1485. doi: 10.13700/j.bh.1001-5965.2015.0464
QUE Jianfeng, WANG Weijun, WU Yuet al. Design of solar-powered aircraft configuration for reducing trim loss[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(7): 1479-1485. doi: 10.13700/j.bh.1001-5965.2015.0464(in Chinese)
Citation: QUE Jianfeng, WANG Weijun, WU Yuet al. Design of solar-powered aircraft configuration for reducing trim loss[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(7): 1479-1485. doi: 10.13700/j.bh.1001-5965.2015.0464(in Chinese)

利于减少配平损失的太阳能飞机构型设计

doi: 10.13700/j.bh.1001-5965.2015.0464
详细信息
    作者简介:

    阙建锋 男 硕士研究生。主要研究方向:太阳能飞机概念设计和建模仿真。E-mail: jfq7708@126.com;王维军 男,博士,副教授。主要研究方向:飞行动力学仿真与控制、微小型飞行器设计试验。Tel.: 010-82317519 E-mail: wangwj@buaa.edu.cn

    通讯作者:

    王维军,Tel.: 010-82317519 E-mail: wangwj@buaa.edu.cn

  • 中图分类号: V221+.2

Design of solar-powered aircraft configuration for reducing trim loss

  • 摘要: 针对具有静稳定性的太阳能飞机一般采用尾翼配平造成气动配平损失的问题,提出了一种“T”构型太阳能飞机。概述该太阳能飞机的总体构型,分析该构型飞机巡航状态下降低重心的自配平原理,建立能量平衡和质量分析模型,给出适合于该构型太阳能飞机的概念设计方法,并优化构型设计参数。结果表明,“T”构型太阳能飞机不仅具有静稳定性,还降低了配平损失。在巡航状态下,“T”构型太阳能飞机单位面积平飞需用功率比常规构型太阳能飞机减少了6.2%,具有明显的应用效果。

     

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出版历程
  • 收稿日期:  2015-07-13
  • 刊出日期:  2016-07-20

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