EI、Scopus 收录
中文核心期刊

留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

旋转钝锥双平面拍摄风洞自由飞试验

蒋增辉 陈农

蒋增辉, 陈农. 旋转钝锥双平面拍摄风洞自由飞试验[J]. 力学学报, 2013, 45(5): 777-781. doi: 10.6052/0459-1879-12-358
引用本文: 蒋增辉, 陈农. 旋转钝锥双平面拍摄风洞自由飞试验[J]. 力学学报, 2013, 45(5): 777-781. doi: 10.6052/0459-1879-12-358
Jiang Zenghui, Chen Nong. WIND TUNNEL FREE-FLIGHT TEST WITH BIPLANAR OPTICAL SYSTEM ON THE SPINNING BLUNT CONE[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(5): 777-781. doi: 10.6052/0459-1879-12-358
Citation: Jiang Zenghui, Chen Nong. WIND TUNNEL FREE-FLIGHT TEST WITH BIPLANAR OPTICAL SYSTEM ON THE SPINNING BLUNT CONE[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(5): 777-781. doi: 10.6052/0459-1879-12-358

旋转钝锥双平面拍摄风洞自由飞试验

doi: 10.6052/0459-1879-12-358
基金项目: 国家自然科学基金资助项目(11202200).
详细信息
    通讯作者:

    蒋增辉,高级工程师,研究方向:非定常空气动力学、超空泡流体动力学.E-mail:jzhhit@163.com

  • 中图分类号: V211.7

WIND TUNNEL FREE-FLIGHT TEST WITH BIPLANAR OPTICAL SYSTEM ON THE SPINNING BLUNT CONE

Funds: The project was supported by the National Natural Science Foundation of China (11202200).
  • 摘要: 在高超声速风洞中开展了双平面拍摄风洞自由飞试验, 对高超声速下(6马赫)旋转钝锥的动稳定特性进 行了研究.采用两光路垂直正交的双平面拍摄光路系统, 实现了对风洞中自由飞行的旋转钝锥在水平和垂直2个平面内飞行姿态的直接同步拍摄和记录, 实现对模型锥形运动在2个平面的直观观察和深入研究.利用双平面同步拍摄的试验数据, 对双平面数据辨识方法进行了研究, 进而获得了模型的静、动导数系数, 给出了判断模型运动稳定性的判据.

     

  • Jiang ZH, Jia QY, Yang YN, et al. Research on conical destabilization. In: Proceeding of the 13th Asian Congress of Fluid Mechanics, Dhaka, Bangladesh, 2010. 141-145
    Lopera J, Terry NT. Coning motion control of a blunt-nose projectile using small deployable strakes. AIAA2007-3812, 2007
    Mao X, Yang S, Xu Y. Coning motion stability of wraparound fin rockets. Science in China Series E: Technological Sciences, 2007, 50(3): 343-350
    姜俊成, 马家驩. 非平面模型自由飞运动及气动参数辨识的数值模拟研究. 空气动力学学报, 1998, 16(2): 232-237 (Jiang Juncheng, Ma Jiahuan. Numerical simulation of non-planar model free flight and the aerodyramic coefficients identification. Acta Aerodynamica Sinica, 1998, 16(2): 232-237 (in Chinese))
    马家驩, 潘文欣, 翟曼玲等. 10°尖锥标模高超声速动导数的实验测量.空气动力学学报, 1997, 15(4): 452-457 (Ma Jiahuan, Pan Wenxin, Zhai Manling, et al. 10° cone model free flight experiment in hypersonic impulse type tunnel for dynamic stability measurement. Acta Aerodynamica Sinica, 1997, 15(4): 452-457 (in Chinese))
    Prislin RH, Holway HP. A wind tunnel free flight testing technique for nonplanar motion of spinning models. AIAA66-774, 1966
    Jaffe P. Nonplanar tests using the wind-tunnel free-flight technique. J Spacecraft, 1973, 10(7): 435-442  
    许可法, 王陵志, 李明娟等. 旋转导弹风洞六自由度自由飞动导数实验研究. 空气动力学学报, 1993, 11(3): 257-262 (Xu Kefa, Wang Lingzhi, Li Mingjuan, et al. Research on dynamic derivative of Spinning missile by six-degree-of-freedom free-flight test in wind tunnel. Acta Aerodynamica Sinica, 1993, 11(3): 257-262 (in Chinese))
    马家驩, 李江, 潘文欣等. 有翼飞行器高超声速动导数的风洞自由飞测量. 流体力学实验与测量, 2001, 15(4): 70-76 (Ma Jiahuan, Li Jiang, Pan Wenxin, et al. Hypersonic pitching damp measurements for a winged vehicle by model free flight. Experiments and Measurements in Fluid Mechanics, 2001, 15(4): 70-76 (in Chinese))
    李江, 马家驩, 潘文欣等. 两种有翼飞行器高超声速动态气动特性的对比实验研究. 空气动力学学报, 2001, 19(2): 70-76 (Li Jiang, Ma Jiahuan, Pan Wenxin, et al. Comparative experiments of two kinds of space shuttle like model for hypersonic pitching damp by model free flight technology. Acta Aerodynamica Sinica, 2001, 19(2): 217-222 (in Chinese))
    Weber DJ. Modification of tricyclic theory for projectile flight dynamics to include the effects of a liquid payload, AIAA 92-0650, 1992
    Ericsson LE. Nonplanar motion effects in free flight around a cone, AIAA Aerospace Sciences Meeting, AIAA 88-0215, 1988
    Winchenbach GL. Aerodynamic testing in a free-flight spark range, XCWL/MN; WL-TR-1997-7006, 1997
    Eikenbery RS. Analysis of the angular motion of missiles. SC-CR-70-6051, 1970
    Lusardi RJ, Nicolaides JD. The determination of non-symmetric aerodynamics of re-entry missiles. AIAA 108, 1974
    Prislin RH. High-amplitude dynamic-stability characteristics of blunt 10-degree cones. AIAA Paper 66-465, 1966
  • 加载中
计量
  • 文章访问数:  1121
  • HTML全文浏览量:  75
  • PDF下载量:  801
  • 被引次数: 0
出版历程
  • 收稿日期:  2013-02-04
  • 修回日期:  2013-05-16
  • 刊出日期:  2013-09-18

目录

    /

    返回文章
    返回