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大展弦比带外挂机翼的颤振分析

许军 马晓平

许军, 马晓平. 大展弦比带外挂机翼的颤振分析[J]. 机械科学与技术, 2015, 34(4): 636-640. doi: 10.13433/j.cnki.1003-8728.2015.0429
引用本文: 许军, 马晓平. 大展弦比带外挂机翼的颤振分析[J]. 机械科学与技术, 2015, 34(4): 636-640. doi: 10.13433/j.cnki.1003-8728.2015.0429
Xu Jun, Ma Xiaoping. Flutter Analysis of a High-aspect-ratio Wing with External Store[J]. Mechanical Science and Technology for Aerospace Engineering, 2015, 34(4): 636-640. doi: 10.13433/j.cnki.1003-8728.2015.0429
Citation: Xu Jun, Ma Xiaoping. Flutter Analysis of a High-aspect-ratio Wing with External Store[J]. Mechanical Science and Technology for Aerospace Engineering, 2015, 34(4): 636-640. doi: 10.13433/j.cnki.1003-8728.2015.0429

大展弦比带外挂机翼的颤振分析

doi: 10.13433/j.cnki.1003-8728.2015.0429
基金项目: 

陕西省自然科学基金项目(2013JM015)资助

详细信息
    作者简介:

    许军(1987-),博士研究生,研究方向为无人机气动弹性,xujun_0516@126.com

    通讯作者:

    马晓平,研究员,博士生导师,maxiaoping@nwpu.edu.cn

Flutter Analysis of a High-aspect-ratio Wing with External Store

  • 摘要: 基于哈密顿原理推导建立大展弦比带外挂机翼的动力学方程。为了分析大展弦比机翼特性,考虑了大展弦比机翼的平面内弯曲效应,将传统机翼的弯扭动力学方程扩展到大展弦比机翼的弯弯扭方程;利用Dirac函数考虑外挂位置的影响;采用拉格朗日乘子的方法考虑梁模型轴向不可伸缩约束。引入无量纲化参数对动力学方程进行无量纲化处理。基于梁模型的边界条件,利用伽辽金方法及主振型的正交性将偏微分方程离散为常微分方程,并改写成矩阵和状态方程的形式。利用K方法进行颤振计算,分析外挂参数如外挂质量、位置和转动惯量对机翼外挂系统颤振速度的影响,并分析了各种速度条件下的响应历程。
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出版历程
  • 收稿日期:  2013-09-16
  • 刊出日期:  2015-04-05

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