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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Research Memorandums
 Collection: Technical Report Archive and Image Library
Wing-flow tests of a triangular wing of aspect ratio two I : effectiveness of several types of trailing-edge flaps on flat-plate models

Wing-flow tests of a triangular wing of aspect ratio two I : effectiveness of several types of trailing-edge flaps on flat-plate models

Date: November 14, 1947
Creator: Rathert, George A , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing load distribution on a swept wing airplane in flight at Mach numbers up to 1.11, and comparison with theory

Wing load distribution on a swept wing airplane in flight at Mach numbers up to 1.11, and comparison with theory

Date: April 14, 1952
Creator: Rolls, L Stewart
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane

Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane

Date: March 30, 1955
Creator: Robinson, Glenn H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing-load measurements of the Bell X-5 research airplane at a sweep angle of 58.7 degrees

Wing-load measurements of the Bell X-5 research airplane at a sweep angle of 58.7 degrees

Date: April 4, 1955
Creator: Banner, Richard D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing loads and load distributions throughout the lift range of the Douglas X-3 research airplane at transonic speeds

Wing loads and load distributions throughout the lift range of the Douglas X-3 research airplane at transonic speeds

Date: November 9, 1956
Creator: Keener, Earl R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing loads on the Bell X-1 research airplane (10 percent thick wing) as determined by pressure-distribution measurements in flight at subsonic and transonic speeds

Wing loads on the Bell X-1 research airplane (10 percent thick wing) as determined by pressure-distribution measurements in flight at subsonic and transonic speeds

Date: November 4, 1953
Creator: Knapp, Ronald J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing-on and wing-off longitudinal characteristics of an airplane configuration having an thin unswept tapered wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4

Wing-on and wing-off longitudinal characteristics of an airplane configuration having an thin unswept tapered wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4

Date: March 14, 1951
Creator: Gillis, Clarence L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing pressure distributions over the lift range of the Convair XF-92A delta-wing airplane at subsonic and transonic speeds

Wing pressure distributions over the lift range of the Convair XF-92A delta-wing airplane at subsonic and transonic speeds

Date: November 30, 1955
Creator: Keeener, Earl R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing pressure distributions over the lift range of the convair xf-92a delta-wing airplane at subsonic and transonic speeds

Wing pressure distributions over the lift range of the convair xf-92a delta-wing airplane at subsonic and transonic speeds

Date: November 30, 1955
Creator: Jordan, G. H.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wing-tunnel investigation at high subsonic speeds of the lateral-control characteristics of an aileron and a stepped spoiler on a wing with leading edge swept back 51.3 degrees

Wing-tunnel investigation at high subsonic speeds of the lateral-control characteristics of an aileron and a stepped spoiler on a wing with leading edge swept back 51.3 degrees

Date: June 7, 1949
Creator: Schneiter, Leslie E
Description: None
Contributing Partner: UNT Libraries Government Documents Department