Boundary Layer Development on a Concave Surface: Flow Visualization and Hot Wire Velocity Measurements
Boundary Layer Development on a Concave Surface: Flow Visualization and Hot Wire Velocity Measurements
摘要
Gortler vortices are key issues in the design of gas turbine blades. The present study deals with flow visualization over concave surface for gas turbine applications. The aim is to comprehend qualitatively the flow trends, particularly the Gortler vortices formation and development. Gortler vortices have the shape of mushroom-like vortices regularly spaced at 25 mm. These vortices grow and increase in strength more rapidly along the surface in the case of the same grid of turbulence applied to the measuring section. The curvature radius of the studied blade is 0.5 m and the stream turbulence intensity level is 2.6%. The velocity field is measured by hot wire anemometer in the streamwise direction. The velocity profile is found to be highly distorted by the momentum transfer associated with Gortler vortices. The results are compared to Blasius flow and to literature data for a blade with curvature radius equal to 2 m.
参考文献16
-
1Gortler, H. 1954. "On the Three-Dimensional Instability of Laminar Boundary Layers on Concave Walls." Nacher, Ges. Wiss. Gottingen 2: 1-26.
-
2Liepmann, H. W. 1943. Investigations on Laminar Boundary Layer Stability and Transition on Curved Boundaries. NACA Wartime report.
-
3Winoto, S. H., and Crane, R. I. 1980. "Vortex Structure in Laminar Boundary Layers on a Concave Wall." Int. J. Heat Fluid Flow 2 (Dec.): 221-31.
-
4Peerhossaini, H., and Wesfreid, J. E. 1988. "On the Inner Structure of Gortler Vortices." Int. J. Heat Fluid Flow 9: 12-8.
-
5Schultz, M. P., and Volino, R. J. 2001. Effects of Concave Curvature on Boundary Layer Transition under High Free-stream Turbulence Conditions, ASME GT-2001-0191.
-
6Winoto, S. H., Shah, D. A., and Mitsudharmadi, H. 2009. "On the Development of Concave Surface Boundary Layer Flows." Presented at the 10th Asian International Conference on Fluid Machinery, Kuala Lumpur, Malaysia.
-
7Hachem, F., and Johnson, M. W. 1990. A Boundary Layer Transition Correlation for Concave Surfaces, ASME 90-GT-222.
-
8Dris, A., and Johnson, M. W. 2005. "Transition on Concave Surfaces." ASME Journal of Turbomachinery 127 (Mar.): 507-11.
-
9Johnson, M. W. 2006. Predicting Transition on Concave Surfaces, ASME GT-2006-90455.
-
10Johnson, M. W. 2011. "Bypass Transition ReceptivityModes." Int. J. Heat and Fluid Flow 32 (Apr.): 392-401.
-
1陈芳,蒋浩康.双斜丝测量三维平均紊流流场方法的改进[J].航空动力学报,1989,4(2):150-154. 被引量:2
-
2WANG Jiadao,CHEN Darong,LI Xiaodi,KONG Xianmei State Key Laboratory of Tribology, Tsinghua University, Beijing 100084, China.Study on design of the regular concave surface profiles[J].Science China Mathematics,2001,44(S1):101-106. 被引量:2
-
3李雨春,蒋浩康.单斜热丝测量叶轮机内三维流动[J].航空动力学报,1989,4(2):145-149. 被引量:2
-
4葛宁.轴流风扇旋转失速时的流场测量与分析[J].航空动力学报,1997,12(1):9-12. 被引量:3
-
5葛宁.轴流风扇旋转失速的实验研究[J].航空动力学报,1995,10(4):357-360.
-
6惠增宏,竹朝霞,郗忠祥,张理,高永卫,尹迪义.全机模型附面层状态红外热像探测研究[J].实验力学,2000,15(4):392-399.
-
7马宏伟,蒋浩康.压气机转子出口流场的发展及三维紊流特性[J].航空动力学报,2000,15(2):113-118. 被引量:11
-
8ATMANI R.,BRIMA A.,ASKOVIC R..STUDY OF THREE-DIMENSIONAL SEPARATION OF BOUNDARY LAYER OVER BLUNT BODIES[J].Journal of Hydrodynamics,2009,21(1):100-107.
-
9马宏伟,蒋浩康.压气机不同状态下转子出口三维紊流流场[J].航空动力学报,1997,12(3):268-272. 被引量:11
-
10Mohd Hazwan bin Yusof,Hiroshi Katanoda,Hiromitsu Morita.Temperature and Pressure Measurements at Cold Exit of Counter-flow Vortex Tube with Flow Visualization of Reversed Flow[J].Journal of Thermal Science,2015,24(1):67-72.