首页> 外文会议>The 26th Congress of International Council of the Aeronautical Sciences (ICAS) including 8th AIAA Aviation Technology, Integration, and Operations Conference (ATIO) >An Experimental and Computational Study of Low Re Number Transitional Flows over an Aerofoil with Leading Edge Slat
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An Experimental and Computational Study of Low Re Number Transitional Flows over an Aerofoil with Leading Edge Slat

机译:具有前缘板条的翼型上低Re数过渡流的实验和计算研究

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