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WER-31: Effect of spanwise blowing on separation and pressure distributions on a thick wing at high angle of attack

Wentz, W. H.
Snyder, Melvin H.
Huffman, R.
Adlib-Yaghmaee, F.
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1985-07
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Technical report
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Turbines,Aerodynamics,Aerofoils
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W.H. Wentz, M.H. Snyder, R. Huffman, and F. Adib-Yaghmaee. Effect of spanwise blowing on separation and pressure distributions on a thick wing at high angle of attack. Wind Energy Report no.31.Wichita State University. Center for Energy Studies, 1985, 101 p.
Abstract
Pressure measurements were made on a section of a full-scale wind turbine blade to investigate the post-separated flow condition at high angles of attack. Airfoil sections on the blade are approximately NACA 23027 to 23030. The tests were conducted in the WSU 7 x 10 ft. Walter Beech Wind Tunnel, at chord Reynolds numbers of $0.5 x 10^6$ To $2.0 x 10^6$, which correspond to Mach numbers of 0.03 to 0.12 respectively. The investigation was conducted by taking surface pressure data and photographs of fluorescent oil flow patterns. Spanwise blowing was provided to simulate possible effects of radial flow on a rotating blade. Blowing momentum coeffi9ients ranged from 0.0 to 0.54, and angles of attack ranged from 10 to 30 degrees. Pressure distributions were integrated to obtain pressure forces. Results show that separation begins at the trailing edge and moves forward progressively as the angle of attack is increased. Spanwise blowing is most effective at angles near stalling. Blowing delays the decrease in post-stall lift, thereby retaining positive axial force to higher angles of attack. Values of Cμ between 0.25 and 0.35 are optimum in terms of increasing lift coefficient. The visualization techniques show that the blowing does not substantially change the separation line location. It is hypothesized that the blowing reduces the size of the separation bubble, resulting in the pressure characteristics observed.
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Wichita State University. Center for Energy Studies
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Wind Energy Report;
;no.31
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