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Y 3.N 21/5:11/L167
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Preliminary tank tests with planing-tail seaplane hulls / |
1 |
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Y 3.N 21/5:11/L168
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A mass-distribution criterion for predicting the effect of control manipulation on the recovery from a spin / |
1 |
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Y 3.N 21/5:11/L169
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Resume of hinge-moment data for unshielded horn-balanced control surfaces / |
1 |
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Y 3.N 21/5:11/L17
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Investigation of effect of sideslip on lateral stability characteristics. : 3 - Rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface / |
1 |
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Y 3.N 21/5:11/L170
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Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane / |
1 |
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Y 3.N 21/5:11/L171
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Analysis of available data on the effectiveness of ailerons without exposed overhang balance / |
1 |
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Y 3.N 21/5:11/L172
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Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil / |
1 |
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Y 3.N 21/5:11/L173
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Column and plate compressive strengths of aircraft structural materials. : Extruded 75S-T aluminum alloy / |
1 |
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Y 3.N 21/5:11/L174
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Hinge moments of sealed-internal-balance arrangements for control surfaces. : 1 - Theoretical investigation / |
1 |
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Y 3.N 21/5:11/L175
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Wind-tunnel investigation of control-surface characteristics. : 21 - Medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.40-airfoil-chord flap on an NACA 0009 airfoil / |
1 |
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Y 3.N 21/5:11/L176
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Tensile tests of NACA and conventional machine-countersunk flush rivets / |
1 |
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Y 3.N 21/5:11/L177
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Climb and high-speed tests of a Curtiss No. 714-1C2-12 four-blade propeller on the Republic P-47C airplane / |
1 |
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Y 3.N 21/5:11/L178
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Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 65(2)-415, 65(3)-418 and 65(4)-421 airfoil sections / |
1 |
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Y 3.N 21/5:11/L179
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Compressibility effects on heat transfer and pressure drop in smooth cylindrical tubes / |
1 |
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Y 3.N 21/5:11/L18
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An infrared cloud indicator. : 1 - Analysis of infrared-radiation exchange with tables and chart for calibration of the cloud indicator / |
1 |
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Y 3.N 21/5:11/L180
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Determination of desirable lengths of Z- and channel-section columns for local-instability tests / |
1 |
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Y 3.N 21/5:11/L181
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Analysis of vertical-tail loads in rolling pull-out maneuvers / |
1 |
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Y 3.N 21/5:11/L182
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The relation between spanwise variations in the critical Mach number and spanwise load distributions / |
1 |
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Y 3.N 21/5:11/L183
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Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation / |
1 |
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Y 3.N 21/5:11/L184
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Experimental verification of the rudder-free stability theory for an airplane model equipped with rudders having negative floating tendency and negligible friction / |
1 |
