Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /
by Jack F. Runckel and Edwin E. Lee, Jr.

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Main Author: Runckel, Jack F.
Related Names: United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration : [1961]
Subjects: Stresses and loads.
Aircraft.
Aerodynamics, aircraft.
Note: Cover title.
"May 1961."
Aerodynamics, aircraft; Aircraft; Stresses and loads.
Physical Description: 93 p. : ill. ; 26 cm.
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