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  5. Passive Shock Wave/Boundary Layer Control of Wing at Transonic Speeds

Passive Shock Wave/Boundary Layer Control of Wing at Transonic Speeds

来源 :第14届亚洲显示会议(The 14th Asian Symposium on Visualization) | 被引量 : 0次 | 上传用户：zhizu81748
【摘 要】
：
At supercritical conditions a porous strip(or slot strip)placed beneath a shock wave can reduce the drag by a weaker lambda shock system,and increase the buffet boundary,even may increase the lift.
【作 者】
：
Ling Zhou Dehua Chen Yang Tao Guangyuan Liu Shuheng Song 
【机 构】
：
China Aerodynamic Research&Development Center,Mianyang 621000,China
【出 处】
：
第14届亚洲显示会议(The 14th Asian Symposium on Visualization)
【发表日期】
：
2017年11期
【关键词】
：
Wing Shock wave/boundary layer interaction Bump Drag reduction Transonic Optimiz 
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　　At supercritical conditions a porous strip(or slot strip)placed beneath a shock wave can reduce the drag by a weaker lambda shock system,and increase the buffet boundary,even may increase the lift.
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