Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4 /
by S.R. Pate.

APA Citation

Pate, S. R.., ARO, I., Arnold Engineering Development Center., United States. Air Force. Systems Command. (1964). Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4. Arnold Air Force Station, Tennessee: Arnold Engineering Development Center, Air Force Systems Command, United States Air Force.

MLA Citation

Pate, S. R., Inc. ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command. Investigation of Drag Reduction by Boundary Layer Suction On a 50-deg Swept Tapered Wing At M (free-stream) = 2.5 to 4. Arnold Air Force Station, Tennessee: Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964.