Call Number (LC) Title Results
Y 3.N 21/5:6/4161 Effect of lubricant base stock on rolling-contact fatigue life / 1
Y 3.N 21/5:6/4162 Study of some burner cross-section changes that increase space-heating rates / 1
Y 3.N 21/5:6/4163 Effect of temperature on rolling-contact fatigue life with liquid and dry powder lubricants / 1
Y 3.N 21/5:6/4164 Two-dimensional diffusion theory analysis of reactivity effects of a fuel-plate-removal experiment / 1
Y 3.N 21/5:6/4165 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
Y 3.N 21/5:6/4166 An experimental and theoretical study of the effect of fuel on pitching-translation flutter / 1
Y 3.N 21/5:6/4167 A rapid method for predicting attached-shock shape / 1
Y 3.N 21/5:6/4168 A method for calculation of hydrodynamic lift for submerged and planing rectangular lifting surfaces / 1
Y 3.N 21/5:6/4169 Atmospheric temperature observations to 100,000 feet for several climatological regions of the Northern Hemisphere / 1
Y 3.N 21/5:6/4170 A reexamination of the use of simple concepts for predicting the shape and location of detached shock waves / 1
Y 3.N 21/5:6/4171 Some ground measurements of the forces applied by pilots to a side-located aircraft controller / 1
Y 3.N 21/5:6/4172 Noise survey under static conditions of a turbine-driven full-scale modified supersonic propeller with an advance ratio of 3.2 / 1
Y 3.N 21/5:6/4173 An analytical investigation of the gust-alleviating properties of a simple pitch damper / 1
Y 3.N 21/5:6/4174 Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high subsonic speeds. : Taper-ratio series / 1
Y 3.N 21/5:6/4175 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
Y 3.N 21/5:6/4176 Effect of flow incidence and Reynolds number on low-speed aerodynamic characteristics of several noncircular cylinders with applications to directional stability and spinning / 1
Y 3.N 21/5:6/4177 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
Y 3.N 21/5:6/4178 Low-speed cascade investigation of compressor blades having loaded leading edges / 1
Y 3.N 21/5:6/4179 Analytical investigation of acceleration restrictiion in a fighter airplane with an automatic control system / 1
Y 3.N 21/5:6/4180 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