Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /
by William A. newsom, Jr.

Description

Main Author: Newsom, William A.
Related Names: United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration : [1962]
Subjects: Stability and control.
Aircraft.
Aerodynamics, aircraft.
Note: Cover title.
"September 1962."
Aerodynamics, aircraft; Aircraft; Stability and control.
Physical Description: 55 p. : ill. ; 26 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign