The longitudinal characteristics at Mach numbers up to 0.92 of a cambered and twisted wing having 40 degrees of sweepback and an aspect ratio of 10
Description: Report presenting an investigation of a sweptback wing in combination with a fuselage of a type considered suitable for long-range, high-speed airplanes in the 12-foot pressure wind tunnel. The investigations included tests of the wing alone, the wing-fuselage combination, and the effects of fences.
Date: September 15, 1952
Creator: Edwards, George G.; Tinling, Bruce E. & Ackerman, Arthur C.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department