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高压捕获翼前缘型线优化和分析

李广利 崔凯 肖尧 徐应洲

李广利, 崔凯, 肖尧, 徐应洲. 高压捕获翼前缘型线优化和分析[J]. 力学学报, 2016, 48(4): 877-885. doi: 10.6052/0459-1879-16-036
引用本文: 李广利, 崔凯, 肖尧, 徐应洲. 高压捕获翼前缘型线优化和分析[J]. 力学学报, 2016, 48(4): 877-885. doi: 10.6052/0459-1879-16-036
Li Guangli, Cui Kai, Xiao Yao, Xu Yingzhou. LEADING EDGE OPTIMIZATION AND PARAMETER ANALYSIS OF HIGH PRESSURE CAPTURING WINGS[J]. Chinese Journal of Theoretical and Applied Mechanics, 2016, 48(4): 877-885. doi: 10.6052/0459-1879-16-036
Citation: Li Guangli, Cui Kai, Xiao Yao, Xu Yingzhou. LEADING EDGE OPTIMIZATION AND PARAMETER ANALYSIS OF HIGH PRESSURE CAPTURING WINGS[J]. Chinese Journal of Theoretical and Applied Mechanics, 2016, 48(4): 877-885. doi: 10.6052/0459-1879-16-036

高压捕获翼前缘型线优化和分析

doi: 10.6052/0459-1879-16-036
基金项目: 国家自然科学基金资助项目(11372324, 11572333).
详细信息
    通讯作者:

    崔凯,副研究员,主要研究方向:高超声速飞行器构型设计.E-mail:kcui@imech.ac.cn

  • 中图分类号: V19;V221+.3;O354.4

LEADING EDGE OPTIMIZATION AND PARAMETER ANALYSIS OF HIGH PRESSURE CAPTURING WINGS

  • 摘要: 为分析翼前缘形状变化对高压捕获翼构型气动性能的影响,基于一种锥体组合捕获翼概念构型,采用幂次函数和余弦函数组合形式对翼前缘型线进行了参数化设计,在比较了多项式和径向基函数两种代理模型的拟合精度基础上,以飞行马赫数7,飞行攻角0° 为计算条件,结合使用均匀实验设计方法、计算流体力学、径向基函数代理模型方法和遗传算法,选择升阻比最大化为目标开展了数值优化,最后基于优化结果进行了单参数的灵敏度分析. 优化结果表明,相对于基准外形而言,优化后构型升力系数增大了约8.1%,阻力系数减小了约12.2%,升阻比提高了约23.4%. 此外,灵敏度分析结果表明升阻比与5 个设计参数均呈非线性关系,其中展向角度对升阻比影响最大,其次为幂次曲线的比例参数,其余3 个参数对升阻比的影响相对较弱.

     

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出版历程
  • 收稿日期:  2016-01-27
  • 修回日期:  2016-05-09
  • 刊出日期:  2016-07-18

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