Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6 /
by Robert J. Mack.

Description

Main Author

Mack, Robert J.

Related Names

Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1974.

Subjects

Camber (Aerofoils)
Lift (Aerodynamics)
Leading edges (Aerodynamics)
Aerodynamics, Supersonic.
Airplanes > Airplanes / Wings > Airplanes / Wings / Testing.

Note

Prepared at Langley Research Center.
Cover title.

Physical Description

49 p. : ill. ; 27 cm.

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