点击下载:《热力学》课程教学资源(PPT课件)Chapter 11 SUBSONIC COMPRESSIBLE FLOW OVER AIRFOILS:LINEAR THEORY(2/2)
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M 2 p,0 p C C = 2 ,0 1− = M C C p p 2 ,0 2 ,0 1 1 − = − = M c c M c c m m l l (11.51)
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点击下载:《热力学》课程教学资源(PPT课件)Chapter 11 SUBSONIC COMPRESSIBLE FLOW OVER AIRFOILS:LINEAR THEORY(2/2)
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