Effects of three spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45° sweptback highly tapered wing at transonic speeds /
by John P. Mugler, Jr.

Description

Main Author: Mugler, John P.
Related Names: Langley Research Center.
Language(s): English
Published: Washington D.C. : National Aeronautics and Space Administration, 1959.
Subjects: Jet fighter planes > Jet fighter planes / Wind tunnel testing.
Transonic wind tunnels > Transonic wind tunnels / Testing.
Stability of airplanes, Longitudinal > Stability of airplanes, Longitudinal / Testing.
Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Testing.
Note: "October, 1959."
Cover title.
Full text also available online. Address as of 11/4/2010:
Physical Description: 40 p. : ill. ; 26 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign