Compressible dynamic stall control using dynamic shape adaptation

被引：5
作者：
Chandrasekhara, MS
Wilder, MC
Carr, LW
机构：
[1] NASA, Ames Res Ctr, React Flow Environm Branch, Moffett Field, CA 94035 USA
[2] USN, Postgrad Sch, NASA, Joint Inst Aeronaut,Dept Aeronaut & Astronaut, Monterey, CA 93943 USA
来源：
AIAA JOURNAL | 2001年 / 39卷 / 10期
关键词：
D O I：
10.2514/2.1196
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Compressible dynamic stall was controlled using dynamic shape adaptation. The flow was found to be dynamic stall vortex free for M=0.3, k=0.05, and α=10 + 1o sin wt deg. The peak suction variation loop over the oscillation cycle was the smallest for the adapting foil.
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页码：2021 / 2024
页数：4
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