A tabulation of section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for four swept wings having the same planform but different surface shapes.
Emma Jean Landrum.

Description

Main Author: Landrum, Emma Jean.
Related Names: United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration : [1962]
Subjects: Stresses and loads.
Stability and control.
Aircraft.
Aerodynamics, missiles and space vehicles.
Aerodynamics, aircraft.
Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Design and construction.
Camber (Aerofoils)
Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Mathematical models.
Note: Cover title.
"April 1962."
Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft; Stability and control; Stresses and loads.
Physical Description: 36 p.: ill. ; 26 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign