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Y 3.N 21/5:6/4162
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Study of some burner cross-section changes that increase space-heating rates / |
1 |
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Y 3.N 21/5:6/4163
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Effect of temperature on rolling-contact fatigue life with liquid and dry powder lubricants / |
1 |
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Y 3.N 21/5:6/4164
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Two-dimensional diffusion theory analysis of reactivity effects of a fuel-plate-removal experiment / |
1 |
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Y 3.N 21/5:6/4165
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Thermal fatigue of ductile materials. : 2 - Effect of cyclic thermal stressing on the stress-rupture life and ductility of S-816 and Inconel 550 / |
1 |
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Y 3.N 21/5:6/4166
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An experimental and theoretical study of the effect of fuel on pitching-translation flutter / |
1 |
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Y 3.N 21/5:6/4167
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A rapid method for predicting attached-shock shape / |
1 |
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Y 3.N 21/5:6/4168
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A method for calculation of hydrodynamic lift for submerged and planing rectangular lifting surfaces / |
1 |
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Y 3.N 21/5:6/4169
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Atmospheric temperature observations to 100,000 feet for several climatological regions of the Northern Hemisphere / |
1 |
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Y 3.N 21/5:6/4170
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A reexamination of the use of simple concepts for predicting the shape and location of detached shock waves / |
1 |
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Y 3.N 21/5:6/4171
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Some ground measurements of the forces applied by pilots to a side-located aircraft controller / |
1 |
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Y 3.N 21/5:6/4172
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Noise survey under static conditions of a turbine-driven full-scale modified supersonic propeller with an advance ratio of 3.2 / |
1 |
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Y 3.N 21/5:6/4173
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An analytical investigation of the gust-alleviating properties of a simple pitch damper / |
1 |
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Y 3.N 21/5:6/4174
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Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high subsonic speeds. : Taper-ratio series / |
1 |
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Y 3.N 21/5:6/4175
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Investigation of deflectors as gust alleviators on a 0.09-scale model of the Bell X-5 airplane with various wing sweep angles from 20 degrees to 60 degrees at Mach numbers from 0.40 to 0.90 / |
1 |
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Y 3.N 21/5:6/4176
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Effect of flow incidence and Reynolds number on low-speed aerodynamic characteristics of several noncircular cylinders with applications to directional stability and spinning / |
1 |
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Y 3.N 21/5:6/4177
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Wind-tunnel investigation of the static longitudinal stability and trim characteristics of a sweptback-wing jet-transport model equipped with an external-flow jet-augmented flap / |
1 |
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Y 3.N 21/5:6/4178
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Low-speed cascade investigation of compressor blades having loaded leading edges / |
1 |
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Y 3.N 21/5:6/4179
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Analytical investigation of acceleration restrictiion in a fighter airplane with an automatic control system / |
1 |
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Y 3.N 21/5:6/4180
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Investigation of spoilers at a Mach number of 1.93 to determine the effects of height and chordwise location on the section aerodynamic characteristics of a two-dimensional wing / |
1 |
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Y 3.N 21/5:6/4181
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Investigation of the effects of propeller diameter on the ability of a flapped wing, with and without boundary layer control, to deflect a propeller slipstream downward for vertical take-off / |
1 |
