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Donald J Graham
发表
High-speed Tests of an Airfoil Section Cambered to Have Critical Mach Numbers Higher than Those Attainable with a Uniform-load Mean Line
Donald J Graham, 1947 .
A systematic investigation of pressure distributions at high speeds over five representative NACA low-drag and conventional airfoil sections
Donald J Graham, R. N. Olsen, Gerald E Nitzberg, 1945 .