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Investigation of Effects of Roughness, Surface Cooling, and Shock Impingement on Boundary-layer Transition on a Two-dimensional Wing
K. R. CzarneckiJohn R. Sevier
出版National Aeronautics and Space Administration, 1960
URLhttp://books.google.com.hk/books?id=vzQkAQAAIAAJ&hl=&source=gbs_api
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