Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /
by Royce L. McKinney and Lloyd S. Jernell.

Description

Main Author

McKinney, Royce L.

Related Names

Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration : 1965.

Subjects

Mach number.
Stability of airplanes, Longitudinal.
Aerodynamic measurements.
Aerodynamic load.

Note

"March 1965."
Cover title.

Physical Description

44 p. : ill. ; 27 cm.

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