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  Partner: UNT Libraries Government Documents Department
 Resource Type: Report
The effect of leading-edge droop upon the pressure distribution and aerodynamic loading characteristics of a 45 degree sweptback wing at transonic speeds

The effect of leading-edge droop upon the pressure distribution and aerodynamic loading characteristics of a 45 degree sweptback wing at transonic speeds

Date: November 8, 1955
Creator: Schmeer, James W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of leading-edge extensions on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail combination having a 40 degree sweptback wing with NACA 64A thickness distribution

The effect of leading-edge extensions on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail combination having a 40 degree sweptback wing with NACA 64A thickness distribution

Date: January 20, 1956
Creator: Sutton, Fred B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of leading-edge-flap deflection on the wing loads, load distributions , and flap hinge moments of the Douglas X-3 research              airplane at transonic speeds

Effect of leading-edge-flap deflection on the wing loads, load distributions , and flap hinge moments of the Douglas X-3 research airplane at transonic speeds

Date: July 15, 1958
Creator: Keener, Earl R; Mcleod, Norman J & Taillon, Norman V
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of leading-edge geometry on boundary-layer transition at Mach 3.1

Effect of leading-edge geometry on boundary-layer transition at Mach 3.1

Date: March 1, 1956
Creator: Brinich, Paul F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6)  to 8.4 x 10(exp 6).

Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6).

Date: November 10, 1948
Creator: Lange, Roy H & May, Ralph W , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds

Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds

Date: November 18, 1955
Creator: Wetzel, Benton E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

Date: July 1, 1945
Creator: Bird, J D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of length-beam on the aerodynamic characteristics of flying-boat hulls

Effect of length-beam on the aerodynamic characteristics of flying-boat hulls

Date: June 1, 1947
Creator: Yates, Campbell C & Riebe, John M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of Length-Beam Ratio on the Aerodynamic Characteristics of Flying-Boat Hulls without Wing Interference

Effect of Length-Beam Ratio on the Aerodynamic Characteristics of Flying-Boat Hulls without Wing Interference

Date: January 16, 1948
Creator: Lowry, John G. & Riebe, John M.
Description: Contains experimental results of an investigation of the aerodynamic characteristics of a family of flying boat hulls of length beam ratios 6, 9, 12, and 15 without wing interference. The results are compared with those taken on the same family of hulls in the presence of a wing.
Contributing Partner: UNT Libraries Government Documents Department
Effect of length-beam ration on resistance and spray of three models of flying-boat hulls

Effect of length-beam ration on resistance and spray of three models of flying-boat hulls

Date: October 1, 1943
Creator: Zeck, Howard
Description: None
Contributing Partner: UNT Libraries Government Documents Department