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Y 3.N 21/5:6/2304
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Effect of heat and power extraction on turbojet-engine performance. : 4 - Analytical determination of effects of hot-gas bleed / |
1 |
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Y 3.N 21/5:6/2305
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An analytical and experimental investigation of the skin friction of the turbulent boundary layer on a flat plate at supersonic speeds / |
1 |
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Y 3.N 21/5:6/2306
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Meteorological analysis of icing conditions encountered in low-altitude stratiform clouds / |
1 |
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Y 3.N 21/5:6/2307
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A theoretical method of determining the control gearing and time lag necessary for a specified damping of an aircraft equipped with a constant-time-lag autopilot / |
1 |
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Y 3.N 21/5:6/2308
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Vibratory stresses in propellers operating in the flow field of a wing-nacelle-fuselage combination / |
1 |
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Y 3.N 21/5:6/2309
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Charts for estimation of longitudinal-stability derivatives for a helicopter rotor in forward flight / |
1 |
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Y 3.N 21/5:6/2310
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Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system / |
1 |
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Y 3.N 21/5:6/2311
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Flight investigation of the variation of static-pressure error of a static-pressure tube with distance ahead of a wing and a fuselage / |
1 |
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Y 3.N 21/5:6/2312
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Bearing strengths of some aluminum-alloy permanent-mold castings / |
1 |
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Y 3.N 21/5:6/2313
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The effects of mass distribution on the low-speed dynamic lateral stability and control characteristics of a model with a 45° sweptback wing / |
1 |
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Y 3.N 21/5:6/2314
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Effect of quadratic terms in differential equations of atmospheric oscillatons / |
1 |
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Y 3.N 21/5:6/2315
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Supersonic lift and pitching moment of thin sweptback tapered wings produced by constant vertical acceleration. : Subsonic leading edges and supersonic trailing edges / |
1 |
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Y 3.N 21/5:6/2316
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Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45° sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain ailerons / |
1 |
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Y 3.N 21/5:6/2317
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Applications of Von Karman's integral method in supersonic wing theory / |
1 |
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Y 3.N 21/5:6/2318
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Full-scale-tunnel investigation of the static-thrust performance of a coaxial helicopter rotor / |
1 |
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Y 3.N 21/5:6/2319
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Some properties of high-purity sintered wrought molybdenum metal at temperatures up to 2400° F / |
1 |
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Y 3.N 21/5:6/2320
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Effects of some solution treatments followed by an aging treatment on the life of small cast gas-turbine blades of a cobalt-chromium-base alloy. |
1 |
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Y 3.N 21/5:6/2321
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Analysis of temperature distribution in liquid-cooled turbine blades / |
1 |
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Y 3.N 21/5:6/2322
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Creep of lead at various temperatures / |
1 |
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Y 3.N 21/5:6/2323
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Theoretical investigation of submerged inlets at low speeds / |
1 |
