Effects of twist and camber and thickness on the aerodynamic characteristics of a 75° swept arrow wing at a mach number of 2.91 /
by James N. Mueller and John E. Grimaud.

Description

Main Author

Mueller, James N.

Related Names

Grimaud, John E.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington [D.C.] : National Aeronautics and Space Administration, [1959]

Subjects

Camber (Aerofoils)
Aerodynamic load.
Airplanes > Airplanes / Wings, Swept-back.

Note

"December 1959."
Cover title.

Physical Description

67 p. : 22 ill. ; 27 cm.

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