Aerodynamic characteristics of two all-movable wings tested in the presence of a fuselage at a Mach number of 1.9
Description: Report presenting testing of half-span models of two wings of different plan form as both all-movable and fixed surfaces in the presence of a half fuselage. All-movable surfaces are being considered for supersonic aircraft as possible angle-of-attack indicators, control surfaces, and all-movable wings. Results regarding the lift characteristics, center of pressure, and drag of the wings are provided.
Date: October 28, 1948
Creator: Conner, D. William
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department