APA (7th ed.) Citation

Daley, B. N., & Lord, D. T. (1955). Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds. National Advisory Committee for Aeronautics.

Chicago Style (17th ed.) Citation

Daley, Bernard N., and Douglas T. Lord. Aerodynamic Characteristics of Several 6-percent-thick Airfoils at Angles of Attack from 0° to 20° at High Subsonic Speeds. Washington, [D.C.]: National Advisory Committee for Aeronautics, 1955.

MLA (9th ed.) Citation

Daley, Bernard N., and Douglas T. Lord. Aerodynamic Characteristics of Several 6-percent-thick Airfoils at Angles of Attack from 0° to 20° at High Subsonic Speeds. National Advisory Committee for Aeronautics, 1955.