A note on the drag due to lift of delta wings at Mach numbers up to 2.0 /
by Robert S. Osborne and Thomas C. Kelly.
APA Citation
Osborne, R. S., Kelly, T. C., Langley Aeronautical Laboratory., United States. National Adviosry Committee for Aeronautics. (1953). A note on the drag due to lift of delta wings at Mach numbers up to 2.0. Washington, D.C.: National Advisory Committee for Aeronautics.
MLA Citation
Osborne, Robert S, Thomas C Kelly, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. A Note On the Drag Due to Lift of Delta Wings At Mach Numbers Up to 2.0. Washington, D.C.: National Advisory Committee for Aeronautics, 1953.
Warning: These citations may not always be complete (especially for serials).