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An Experimental Investigation of the Zero-lift-drag Characteristics of Symmetrical Blunt-trailing Edge Airfoils at Mach Numbers from 2.7 to 5.0

出版	National Advisory Committee for Aeronautics, 1953
URL	http://books.google.com.hk/books?id=6WvTSgAACAAJ&hl=&source=gbs_api