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A Correlation of Experimental Zero-lift Drag of Rectangular Wings with Symmetrical NACA 65-series Airfoil Sections by Means of the Transonic Similarity Law for Wings of Finite Aspect Ratio
出版NACA, 1951
URLhttp://books.google.com.hk/books?id=ii4UyAEACAAJ&hl=&source=gbs_api