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Y 3.N 21/5:11/L299
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Lift and drag data for 30 pusher-propeller shaft housings on an NACA 65,3-018 airfoil section / |
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Y 3.N 21/5:11/L3
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A method for determining oil-cooler performance requirements in series operation / |
1 |
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Y 3.N 21/5:11/L30
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The use of geared spring tabs for elevator control / |
1 |
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Y 3.N 21/5:11/L301
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Wind-tunnel investigated of control-surface characteristics. : 3 - A small aerodynamic balance of various nose shapes used with a 30-percent-chord flap on an NACA 0009 airfoil / |
1 |
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Y 3.N 21/5:11/L302
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A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls / |
1 |
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Y 3.N 21/5:11/L303
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Test of a dual-rotation axial-flow fan / |
1 |
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Y 3.N 21/5:11/L304
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The effect of solidity, blade section, and contravane angle on the characteristics of an axial-flow fan / |
1 |
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Y 3.N 21/5:11/L305
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The effects of angle of dead rise and angle of afterbody keel on the resistance of a model of a flying-boat hull / |
1 |
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Y 3.N 21/5:11/L306
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The effect of dead rise upon the high-angle porpoising characteristics of two planing surfaces in tandem / |
1 |
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Y 3.N 21/5:11/L307
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Shear-lag tests of two box beams with flat covers loaded to destruction / |
1 |
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Y 3.N 21/5:11/L308
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Theory of self-excited mechanical oscillations of hinged rotor blades / |
1 |
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Y 3.N 21/5:11/L309
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Some theoretical considerations of longitudinal stability in power-on flight with special reference to wind-tunnel testing / |
1 |
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Y 3.N 21/5:11/L31
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Aerodynamic tests of a full-scale TBF-1 aileron installation in the Langley 16-foot high-speed tunnel / |
1 |
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Y 3.N 21/5:11/L310
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Comparison of an approximate and an exact method of shear-lag analysis / |
1 |
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Y 3.N 21/5:11/L311
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Wind-tunnel tests of two tapered wings with straight leading edges and with constant-chord center secitons of different spans / |
1 |
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Y 3.N 21/5:11/L312
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Theory of mechanical oscillations of rotors with two hinged blades / |
1 |
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Y 3.N 21/5:11/L313
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On the plane potential flow past a lattice of arbitrary airfoils / |
1 |
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Y 3.N 21/5:11/L314
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Wind-tunnel investigation of control-surface characteristics. : 13 - Various flap overhangs used with a 30-percent-chord flap on an NACA 66-009 airfoil / |
1 |
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Y 3.N 21/5:11/L315
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Effect of countersunk depth on the tightness of two types of machine-countersunk rivet / |
1 |
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Y 3.N 21/5:11/L316
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Wind-tunnel tests of single- and dual-rotating tractor propellers at low blade angles and of two- and three-blade tractor propellers at blade angles up to 65 degrees / |
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