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Experimental Study of Dynamic Stall on Advanced Airfoil Sections. Volume 3:Hot-Wire and Hot Film Measurements.

机译:先进翼型截面动态失速的试验研究。第3卷:热线和热膜测量。

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摘要

Detailed unsteady boundary layer measurements are presented for eight airfoils oscillated in pitch through the dynamic stall regime. The present report (the third of three volumes) describes the techniques developed for analysis and evaluation of the hot film and hot wire signals, offers some interpretation of the results, and tabulates all the cases in which flow reversal has been recorded.

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