Oscillating pressures near a static pusher propeller at tip Mach numbers up to 1.20 with special reference to the effects of the presence of the wing /
Harvey H. Hubbard and Leslie W. Lassiter.

APA Citation

Hubbard, H. H., Lassiter, L. W., United States. National Advisory Committee for Aeronautics. (1954). Oscillating pressures near a static pusher propeller at tip Mach numbers up to 1.20 with special reference to the effects of the presence of the wing. Washington, D.C.: National Advisory Committee for Aeronautics.

MLA Citation

Hubbard, Harvey H, Leslie W Lassiter, and United States. National Advisory Committee for Aeronautics. Oscillating Pressures Near a Static Pusher Propeller At Tip Mach Numbers Up to 1.20 With Special Reference to the Effects of the Presence of the Wing. Washington, D.C.: National Advisory Committee for Aeronautics, 1954.