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.

Description

Main Author

Osborne, Robert S.

Related Names

Kelly, Thomas C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1953.

Subjects

Airplanes > Airplanes / Wings, Triangular.
Lift (Aerodynamics)
Drag (Aerodynamics)

Note

"April 9, 1953."

Physical Description

14 p. : ill. ; 27 cm.

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