Longitudinal trim characteristics of a deflected slipstream V/Stol aircraft during level flight at transition flight speeds /
Howard L. Turner and Fred J. Drinkwater III.

Description

Main Author: Turner, Howard L.
Related Names: Drinkwater, Fred J.
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.
"October 1962."
Aerodynamics, aircraft; Aircraft; Stability and control.
Physical Description: 19 p.: ill. ; 26 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign