Application of variable leading-edge roughness for transition control on swept wings
摘要：
For transition to turbulence in crossflow-dominated swept-wing boundary layers, details of the strongly nonlinear nature of the stationary primary instability are well understood both experimentally and theoretically. It is the particular action of the
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会议名称：
38th Aerospace Sciences Meeting and Exhibit
会议时间：
2000
被引量：
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