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 .