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Y 3.N 21/5:11/L292
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Effects of a simulated ice formation on the aerodynamic characteristics of an airfoil / |
1 |
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Y 3.N 21/5:11/L293
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Tests of hydraulically expanded rivets / |
1 |
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Y 3.N 21/5:11/L294
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A study of the tightness and flushness of machine-countersunk rivets for aircraft / |
1 |
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Y 3.N 21/5:11/L295
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Wind-tunnel tests of a twin-engine model to determine the effect of direction of propeller rotation on the static-stability characteristics / |
1 |
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Y 3.N 21/5:11/L296
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Tapered wings, tip stalling, and preliminary results from tests of the stall-control flap / |
1 |
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Y 3.N 21/5:11/L297
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Comparative tests of the strength and tightness of commercial flush rivets of one type and NACA flush rivets in machine-countersunk and counterpunched joints / |
1 |
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Y 3.N 21/5:11/L298
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Use of stagnation temperature in calculating rate of heat transfer in aircraft heat exchangers / |
1 |
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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 / |
1 |
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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 |
