Full-scale wind-tunnel and flight tests of a Fairchild XR2K-1 airplane with a Zap flap and upper-surface aileron-wing installation / by L.A. Clousing, Robert R. Lehr, and William J. O'Sullivan.
A Fairchild XR2K-1 airplane equipped with a wing having a full-span Zap flap and upper-surface ailerons was tested in the full-scale wind tunnel and in flight to determine the characteristics of the flap and the ailerons. The lift, drag, and pitching-moment coefficients of the airplane and the ailer...
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| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Other Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1942]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L437. |
| Subjects: |
Search Result 1
Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades /
Published 1946
Government Document
Book
Search Result 2
Aerodynamic characteristics of several modifications of a 0.45-scale model of the vertical tail of the Curtiss XP-62 airplane /
Published 1946
Government Document
Book
Search Result 3
Aerodynamic data for a wing section of the Republic XF-12 airplane equipped with a double slotted flap /
Published 1946
Government Document
Book
Search Result 4
Analysis of effect of rolling pull-outs on wing and aileron loads of a fighter plane /
Published 1946
Government Document
Book
Search Result 5
An analysis of the fatigue life of an airplane wing structure under overload conditions /
Published 1946
Government Document
Book
Search Result 6
An analysis of the indications of the University of Chicago airborne turbulence indicator in gusty air /
Published 1946
Government Document
Book
Search Result 7
Search Result 8
Approximate formulas for the computation of turbulent boundary-layer momentum thicknesses in compressible flows /
Published 1946
Government Document
Book
Search Result 9
Calibrations of service pitot tubes in the Langley 24-inch high-speed tunnel /
Published 1946
Government Document
Book
Search Result 10
Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates /
Published 1946
Government Document
Book
Search Result 11
Column and plate compressive strengths of aircraft structural materials. : Extruded 14S-T aluminum alloy /
Published 1946
Government Document
Book
Search Result 12
Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel /
Published 1946
Government Document
Book
Search Result 13
Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane /
Published 1946
Government Document
Book
Search Result 14
A correlation of loadings and afterbody length-beam ratios of various flying-boat hulls /
Published 1946
Government Document
Book
Search Result 15
Correlation tests of the ditching behavior of an Army B-24D airplane and a 1/16-size model /
Published 1946
Government Document
Book
Search Result 16
Critical combinations of longitudinal and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation /
Published 1946
Government Document
Book
Search Result 17
Determination of induced velocity in front of an inclined propeller by a magnetic-analogy method /
Published 1946
Government Document
Book
Search Result 18
Determination of the stability and control characteristics of a straight-wing, tailless fighter-airplane model in the Langley free-flight tunnel /
Published 1946
Government Document
Book
Search Result 19
Determination of towline tension and stability of spin-recovery parachutes /
Published 1946
Government Document
Book
Search Result 20
