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Y 3.N 21/5:11/L460
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On a function-theory method for obtaining potential-flow patterns of a compressible fluid / |
1 |
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Y 3.N 21/5:11/L461
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Influence of loading condition on piloting technique for spin recovery for pursuit airplanes / |
1 |
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Y 3.N 21/5:11/L462
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Investigation of drag and pressure distribution of windshields at high speeds / |
1 |
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Y 3.N 21/5:11/L463
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Tests of a large spherical turret and a modified turret on a typical bomber fuselage / |
1 |
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Y 3.N 21/5:11/L464
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Wind-tunnel investigation of control-surface characteristics. : 5 - The use of a beveled trailing edge to reduce the hinge moment of a control surface / |
1 |
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Y 3.N 21/5:11/L465
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A study of the effect of adverse yawing moment on lateral maneuverability at a high lift coefficient / |
1 |
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Y 3.N 21/5:11/L466
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Critical stresses for plates / |
1 |
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Y 3.N 21/5:11/L467
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Adjustment of stick force by a nonlinear aileron-stick linkage / |
1 |
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Y 3.N 21/5:11/L468
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The longitudinal stability of flying boats as determined by tests of models in the NACA tank. : 2 - Effect of variations in form of hull on longitudinal stability / |
1 |
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Y 3.N 21/5:11/L469
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Wind-tunnel investigation of an NACA 23012 airfoil with a 0.30-airfoil-chord double slotted flap / |
1 |
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Y 3.N 21/5:11/L47
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Wind-tunnel investigation of control-surface characteristics. : 23 - A 0.25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 airfoil / |
1 |
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Y 3.N 21/5:11/L470
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Wind-tunnel investigation of a plain aileron with various trailing-edge modifications on a tapered wing. : 3 - Ailerons with simple and spring-linked balancing tabs / |
1 |
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Y 3.N 21/5:11/L471
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Aerodynamic characteristics of a 4-engine monoplane showing comparison of air-cooled and liquid-cooled engine installations / |
1 |
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Y 3.N 21/5:11/L472
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The longitudinal shear strength required in double-angle columns of 24S-T aluminum alloy / |
1 |
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Y 3.N 21/5:11/L473
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A simplified chart for determining Mach number and true airspeed from airspeed-indicator readings / |
1 |
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Y 3.N 21/5:11/L474
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Condensation trails. : Where they occur and what can be done about them / |
1 |
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Y 3.N 21/5:11/L475
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Tank tests of a 1/5 full-size dynamically similar model of the Army OA-9 amphibian with motor-driven propellers -- NACA model 117 / |
1 |
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Y 3.N 21/5:11/L476
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Critical shear stress of an infinitely long flat plate with equal elastic restraints against rotation along the parallel edges / |
1 |
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Y 3.N 21/5:11/L477
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NACA radio ground-speed system for aircraft / |
1 |
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Y 3.N 21/5:11/L478
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Ground-cooling and flight tests of an airplane equipped with a nose-blower engine cowling / |
1 |
