Effect of wing leading-edge shape on aerodynamic characteristics of a 67 ̊swept wing-body model at Mach 1.50 to 4.63 /
Robert G. Kyle and Maurice O. Feryn.

Description

Main Author

Kyle, Robert G.

Related Names

Feryn, Maurice O.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration : 1966.

Subjects

Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Aerodynamics.

Physical Description

22 p. : ill. ; 27 cm.

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