期刊文献+

激光测速测量湍流分离-再附流动 被引量:4

LDV MEASUREMENT OF A TURBULENT SEPARATION-REATTACHMENT FLOW
下载PDF
导出
摘要 湍流边界层分离研究是当前流体力学中难度极大的课题。有关的试验比较罕见,其重要原因是接触式测速技术对流场有干扰且无方向敏感性,因而难以获得可信数据。激光多普勒测速(LDV)作为非接触测速技术,可以有效地测量间歇反流特征,因此越来越多的研究者倾向于应用LDV研究湍流分离流。迄今为止,应用LDV对分离流的研究一般侧重于分离过程。对整个湍流分离-再附过程进行完整的测量尚不多见。本试验采用二维LDV系统详细地测量了二维非对称曲壁扩压器内的湍流分离-再附流动。 Detailed investigation of a turbulent separation-reatta-chment flow in a 2-D curved-wall diffuser using TSI model 9100-7, two-color, dual-beam Laser Doppler Velocimeter System. This separation occurs under strong adverse pressure gradient on a convex surface with large curvature, and the separated shear layer reattaches downstream where the adverse pressure gradient becomes milder or under the natural relaxation condition, simulating the actual flows in some engineering applications.Mean velocities U, V and Reynolds stresses u2, v2 and -uv are presented. The preliminary analysis shows that the experimental results are reliable. The entire flow field can be divided into five regions. The reatiaching flow is about twice the length of the separating zone. Due to the separation, the streamwise curvature induces a significant normal pressure gradient near the incipient detachment. It is found that there exists a second peak on u2, as well as a negative of (-uv ) having the same order of magnitude as (-uv)max, downstream of the transitory detachment.
机构地区 南京航空学院
出处 《航空学报》 EI CAS CSCD 北大核心 1990年第5期A257-A261,共5页 Acta Aeronautica et Astronautica Sinica
关键词 激光测速 湍流 分离流 再附流 测量 laser anemometer, turbulent flow, separated flow, reattaching flow.
  • 相关文献

同被引文献24

  • 1齐鄂荣,黄明海,李炜,张昕.二维后向台阶流流动特性的实验研究[J].实验力学,2006,21(2):225-232. 被引量:9
  • 2连淇祥.后向台阶湍流拟序结构的实验研究[J].力学学报,1993,25(2):129-133. 被引量:8
  • 3韩振兴,邸倩倩,李志宏,刘石.热敏液晶定量测温系统[J].仪器仪表学报,2006,27(7):679-682. 被引量:3
  • 4陈钊,郭永彩,高潮.三维PIV原理及其实现方法[J].实验流体力学,2006,20(4):77-82. 被引量:25
  • 5Hoson H P. Boundary-Layer Transition and Separation near the Trailing Edge of High-Speed Turbine Blade. ASME Journal of Engineering for Power, 1985, 106: 391- 399.
  • 6I Popovic, J Zhu, W Dai, et al. Aerodynamics of a Family of Three Highly Loaded Low-Pressure Turbine Airfoils: Measured Effects of Reynolds Number and Turbulence Intensity in Steady Flow. ASME, 2006, No.GT2006-91271.
  • 7Bellhouse B J, Schultz D L. Determination of Mean and Dynamic Skin Friction, Separation and Transition in Low-Speed Flow with a Thin-Film Heated Element. Journal of Fluid Mechanics, 1966, 24:379-400.
  • 8Hodson H P. Measurements of Wake-Generated Unsteadiness in the Rotor Passage of Axial Flow Turbines. ASME Journal of Engineering for Gas Turbines and Power, 1985, 107:467-476.
  • 9Ali Mahallati. Aerodynamics of a Low-Pressure Turbine Airfoil Under Steady and Periodically Unsteady conditions: [Ph,D. Thesis]. Canada: Carleton University, 2003.
  • 10王明杰,雷志军,朱俊强.压气机叶片附面层转捩的试验研究[J].工程热物理学报,2008,29(3):419-422. 被引量:6

引证文献4

二级引证文献18

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部