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不同头部形状单孔位微吹气扰动控制实验研究
引用本文:孙淑园,邓学蓥,詹慧玲.不同头部形状单孔位微吹气扰动控制实验研究[J].北京航空航天大学学报,2005,31(6):599-603.
作者姓名:孙淑园  邓学蓥  詹慧玲
作者单位:北京航空航天大学 航空科学与工程学院, 北京 100083
基金项目:国家自然科学基金,航空科研项目,武器装备预研基金
摘    要:在亚临界流动范围内,对具有不同头部形状的尖拱形细长旋成体在无侧滑大迎角下进行单孔位微吹气扰动控制实验.通过对物面压力分布、截面侧向力分布和以前细长旋成体结果的对比和分析,发现单孔位微吹气扰动对于细长旋成体横侧向控制作用在于模型头部背风侧非对称二涡结构对扰动的敏感性.实验分析表明,单孔位微吹气扰动这一大迎角非对称控制手段具有较强的适应能力,其控制能力的大小则由该头部形状的初始状态决定.

关 键 词:细长体  空气动力学  非对称涡  前体涡控制
文章编号:1001-5965(2005)06-0599-05
收稿时间:2004-01-12
修稿时间:2004年1月12日

Study of flow control over different noses with single hole microblowing
Sun Shuyuan,Deng Xueying,Zhan Huiling.Study of flow control over different noses with single hole microblowing[J].Journal of Beijing University of Aeronautics and Astronautics,2005,31(6):599-603.
Authors:Sun Shuyuan  Deng Xueying  Zhan Huiling
Institution:School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:The SHM(single hole microblowing) as a new perturbation active control technique has been applied to the slender body with different model noses at zero sideslip and high angle of attack. The analyzed and contrasted results of the distribution of the surface pressure distributions and the sectional side forces with the former results of the slender body in the same flow conditions show that the SHM's control effect to the slender body is due to that the two asymmetric vortices over the slender body model are sensitive to the nose perturbations. The analyses indicate that the SHM's control ability has strong adaptability to various slender body at high angles of attack, and its control ability is determined by the original state of the flowfield around the slender body.
Keywords:slender body  aerodynamics  asymmetric vortices flow  forebody vortex control
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