Measurements in a turbine cascade flow under ultra low Reynolds number conditions

被引:35
作者
Van Treuren, KW [1 ]
Simon, T
von Koller, M
Byerley, AR
Baughn, JW
Rivir, R
机构
[1] Baylor Univ, Dept Engn, Waco, TX 76798 USA
[2] Univ Minnesota, Dept Mech Engn, Minneapolis, MN 55455 USA
[3] Bundesamt Wehrtech & Beschaffung, Koblenz, Germany
[4] USAF Acad, Dept Aeronaut, Colorado Springs, CO 80840 USA
[5] Univ Calif Davis, Davis, CA 95616 USA
[6] USAF, Wright Labs, Aero Prop & Power Directorate, Wright Patterson AFB, OH 45433 USA
来源
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 2002年 / 124卷 / 01期
关键词
turbine cascade; low Reynolds number flow;
D O I
10.1115/1.1415736
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
With the new generation of gas turbine engine, low Reynolds number flows have become increasingly important. Designers must properly account for, transition front laminar to turbulent flow, and separation of the flow, front the suction surface, which is strongly dependent upon transition. Of interest to industry, are Reynolds numbers based upon suction surface length and flow, exit velocity below 150,000 and as low as 25,000. In this paper, the extreme low end of this Reynolds number range is documented by way of pressure distributions, loss coefficients, and identification of separation zones. Reynolds numbers of 25,000 and 50,000 and with I percent and 8-9 percent turbulence intensity of the approach flow (free-stream turbulence intensity, FSTI) were investigated, At 25,000 Reynolds number and low FSTI. the suction surface displayed a strong and steady separation region. Raising the turbulence intensity resulted in a very unsteady separation region of nearly the same size on the suction surface, Vortex generators were added to the suction surface, but they appeared to do very little at this Reynolds number At the higher Reynolds number of 50,000, the low-FSTI case was strongly separated on the downstream portion of the suction surface. The separation zone was eliminated when the turbulence level was increased to 8-9 percent. Vortex generators were added to the suction surface of the low-FSTI case. In this instance, the vortices it-ere able to provide the mixing needed to re-establish flow attachment. This paper shows that massive separation at very, low Reynolds numbers (25,000) is persistent, in spite of elevated FSTI and added vortices. However, at a higher Reynolds number; there is opportunity for flow, reattachment either with elevated free-stream turbulence or with added vortices. This may be the first documentation of flow behavior at such low, Reynolds numbers. Although it is undesirable to operate under these conditions. it is important to know what to expect and how performance may be improved if such conditions tire unavoidable.
引用
收藏
页码:100 / 106
页数:7
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