Wind-tunnel investigation of control-surface characteristics. : 18 - A linked overhang aerodynamic balance / by Richard I. Sears and Robert B. Liddell.
Wind-tunnel tests have been made in two-dimensional flow to investigate the aerodynamic characteristics of a flap balanced by a large overhang linked to deflect more slowly than the flap. Three lengths of blunt-nose overhang were tested linked to a 0.30-airfoil-chord straight-contour flap on an NACA...
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| Main Author: | |
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| 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,
[1944]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L350. |
| Subjects: |
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Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades /
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Aerodynamic characteristics of several modifications of a 0.45-scale model of the vertical tail of the Curtiss XP-62 airplane /
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Aerodynamic data for a wing section of the Republic XF-12 airplane equipped with a double slotted flap /
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Analysis of effect of rolling pull-outs on wing and aileron loads of a fighter plane /
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An analysis of the fatigue life of an airplane wing structure under overload conditions /
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An analysis of the indications of the University of Chicago airborne turbulence indicator in gusty air /
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Approximate formulas for the computation of turbulent boundary-layer momentum thicknesses in compressible flows /
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Calibrations of service pitot tubes in the Langley 24-inch high-speed tunnel /
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Charts for critical combinations of longitudinal and transverse direct stress for flat rectangular plates /
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Column and plate compressive strengths of aircraft structural materials. : Extruded 14S-T aluminum alloy /
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Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel /
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Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane /
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A correlation of loadings and afterbody length-beam ratios of various flying-boat hulls /
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Correlation tests of the ditching behavior of an Army B-24D airplane and a 1/16-size model /
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Critical combinations of longitudinal and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation /
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Determination of induced velocity in front of an inclined propeller by a magnetic-analogy method /
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Determination of the stability and control characteristics of a straight-wing, tailless fighter-airplane model in the Langley free-flight tunnel /
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Determination of towline tension and stability of spin-recovery parachutes /
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Search Result 20
