A study of the effects of vertical tail area and dihedral on the lateral maneuverability of an airplane / by Leo F. Fehlner.
A theoretical investigation has been made of the influence of changes in vertical tail area and dihedral angle on the lateral flying characteristics of an airplane. The lateral motions were computed for nine different combinations of vertical tail area and dihedral, covering the range of parameters...
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| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1941]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L347. |
| 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 /
Published 1946
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Search Result 20
