期刊文献+

迎角变化对细长旋成体绕流非定常压力脉动特征的影响 被引量:1

The impact of variant attack of angle on the unsteady pressure fluctuation characteristics of the flow over slender body
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摘要 在亚临界流动范围内,通过对尖拱细长旋成体在无侧滑状态下的烟线显示和脉动压力测量试验,揭示了迎角α从0°向90°变化过程中细长体绕流依次经历了四种背涡流动结构:附着流动、对称二涡结构、非对称多涡结构和混合背涡结构。压力的脉动幅度在附着流动和对称二涡结构中沿轴向基本保持不变,在非对称多涡结构中是沿轴向增长的,而在混合背涡结构中却变为沿轴向减少。压力脉动频率值在非对称多涡结构中是沿轴向减少的,而在混合背涡结构中却是沿轴向增长的。 Tests of sharp ogive nose cylinders at variant angle of attack with smoke visualization and pressure fluctuation measurement have been carried out in subcritical Reynolds number region. As the angle of attack α increasing from 0° to 90°, there are four kinds of vortices structure and they are attaching flow structure.twin vortices structure.asymmetric vortices structure and mixed vortices structure in turn. The pressure fluctuation magnitude alone the axis is unchanged in attaching flow structure and twin vortices structure, increasing in asymmetric vortices structure, and decreasing in mixed vortices structure. The pressure fluctuation frequency alone the axis is decreasing in asymmetric vortices structure, and increasing in mixed vortices structure.
出处 《实验流体力学》 CAS CSCD 北大核心 2008年第2期15-19,共5页 Journal of Experiments in Fluid Mechanics
基金 国家自然科学基金(1072017) 航空基础科学基金(02A51048) 翼型叶栅空气动力学国防科技重点实验室基金(00JS51.3.2HK01)资助项目
关键词 旋成体 非对称背涡 压力脉动 流动显示 body of revolution asymmetric vortices pressure fluctuation flow visualization
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参考文献7

  • 1LAMONT P J, HUNT B L. Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream [ J ] . Journal of Fluid Mechanics, 1976, 76: 519-559.
  • 2HUNT B L, DEXTER P C. Pressures on a slender body at high angle of attack in a very low turbulence level air stream [R]. AGARD CP 247, 1979.
  • 3WARDLAW A B, YANTA W J. The flow field about and forces on slender bodies at high angles of attack[R]. AIAA 80- 0184.
  • 4DEGANI D, ZILLIAC G G. Experimental study of nonsteady asymmetric flow around an ogive-cylinder at incidence[J]. AIAA Journal, 1990, 28: 642-649.
  • 5TELIONIS D P, ZEIGER M D, VLACHOS P P. Unsteady separated flows over 3-D slender bodies[ R]. AIAA 99-3693.
  • 6刘沛清,邓学蓥,孔繁美.绕细长旋成体非对称涡非定常性的实验研究[J].流体力学实验与测量,2002,16(4):39-46. 被引量:5
  • 7邓学蓥,王刚,陈学锐,王延奎,刘沛清.细长旋成体大迎角正则态非对称涡系结构的物理模型(邀请报告)[A].第五届全国流动显示学术会议论文集[C],2002.

二级参考文献7

  • 1[1]LAMONT P J,HUNT B L.Pressure and force distributions on a sharp nose circular cylinder at large angles of inclinations to uniform subsonic stream.Journal of Fluid Mechanics,1976,76(3):519~559.
  • 2[2]DEGANI D,ZILLIAC G G.Experimental study of nonsteady asymmetric flow around an ogive cylinder at incidence.AIAA Jorunal 1990,28(4):642~649.
  • 3[3]ERICSSON L E.Vortex unsteadiness on slender bodies at high incidence.Journal of Spacecraft,1987,24(4):319~326.
  • 4[4]YANTA W J,WARDLAW A B.Flowfield about and forces on slender bodies at high angles of attack.AIAA Journal,1981,19(3):296~302.
  • 5[5]KEENER E R,CHAPMAN G T.Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack.AIAA Paper,No.74~770,1974.
  • 6[6]LUO S C,LIM T T,LUA K B,et al.Flowfield around ogive/elliptic-tip cylinder at high angle of attack.AIAA Journal,1998,36(10):1778~1787.
  • 7[7]BLOOR S M.The transition to turbulence in the wake of a circular cylinder.Journal of Fliud mechanics,1964,19(期),290~304.

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