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Y 3.N 21/5:11/L779
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Wind-tunnel tests of the 1/9-scale model of the Curtiss XP-62 airplane with various vertical tail arrangements / |
1 |
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Y 3.N 21/5:11/L78
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A simple method for estimating terminal velocity including effect of compressibility on drag / |
1 |
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Y 3.N 21/5:11/L780
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Analytical investigation of the stability of an F8F dropping model with automatic stabilization / |
1 |
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Y 3.N 21/5:11/L781
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Estimation of critical speeds of airfoils and streamline bodies / |
1 |
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Y 3.N 21/5:11/L782
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A method for correlating the cooling data of liquid-cooled engines and its application to the Allison V-3420-11 engine / |
1 |
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Y 3.N 21/5:11/L783
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Free-spinning-tunnel tests of a 1/23.75-scale model of the Douglas DC-3 airplane / |
1 |
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Y 3.N 21/5:11/L784
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Effects of propellers and of vibration on the extent of laminar flow on the NACA 27-212 airfoil / |
1 |
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Y 3.N 21/5:11/L785
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Wind-tunnel tests of the 0.15-scale powered model of the Fleetwings XBTK-1 airplane. : Longitudinal stability and control / |
1 |
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Y 3.N 21/5:11/L786
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Wind-tunnel tests of the 0.15-scale powered model of the Fleetwing XBTK-1 airplane. : Lateral stability and control / |
1 |
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Y 3.N 21/5:11/L787
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Wind-tunnel tests of the 1/8-scale powered model of the Curtiss XBTC-2 airplane. : 2 - Preliminary investigation of lateral stability and control / |
1 |
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Y 3.N 21/5:11/L79
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Resistance tests of models of three flying-boat hulls with a length-beam ratio of 10.5 / |
1 |
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Y 3.N 21/5:11/L8
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Investigation of effect of sideslip on lateral stability characteristics. : 2 - Rectangular midwing of 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/L80
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Wind-tunnel tests of dual-rotating propellers with systematic differences in number of blades, blade setting, and rotational speed of front and rear propellers / |
1 |
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Y 3.N 21/5:11/L81
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A solution of the direct and inverse potential problems for arbitrary cascades of airfoils / |
1 |
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Y 3.N 21/5:11/L82
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Effects of Reynolds number and leading-edge roughness on lift and drag characteristics of the NACA 65,3-418, a = 1.0 airfoil section / |
1 |
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Y 3.N 21/5:11/L83
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Comparison of yaw characteristics of a single-engine airplane model with single-rotating and dual-rotating propellers / |
1 |
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Y 3.N 21/5:11/L84
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Low-pressure boundary-layer control in diffusers and bends / |
1 |
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Y 3.N 21/5:11/L85
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Use of variable-ratio geared tabs to improve stick-force characteristics in turning flight / |
1 |
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Y 3.N 21/5:11/L86
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Fight investigation of boundary-layer and profile-drag characteristics of smooth wing sections of a P-47D airplane / |
1 |
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Y 3.N 21/5:11/L87
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A comparison of data obtained by two flight techniques for determining the sideslip characteristics of a fighter airplane / |
1 |
