Call Number (LC) Title Results
Y 3.N 21/5:11/E17 Compressibility and heating effects on pressure loss and cooling of a baffled cylinder barrel / 1
Y 3.N 21/5:11/E170 Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine. : 1 - Description of setup and testing technique / 1
Y 3.N 21/5:11/E171 Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine. : 2 - Determination of the limiting-icing conditions / 1
Y 3.N 21/5:11/E172 Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine. : 3 - Heated air as a means of de-icing the carburetor and supercharger inlet elbow / 1
Y 3.N 21/5:11/E173 Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine. : 4 - Effect of throttle design and method of throttle operation on induction-system icing characteristics / 1
Y 3.N 21/5:11/E174 Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine. : 5 - Effect of injection of water-fuel mixtures and water-ethanol - fuel mixtures on the icing characteristics / 1
Y 3.N 21/5:11/E175 Laboratory investigation of icing in the carburetor and supercharger inlet elbow of an aircraft engine. : 6 - Effect of modifications to fuel-spray nozzle on icing characteristics / 1
Y 3.N 21/5:11/E176 Investigation of ice formation in the induction system of an aircraft engine. : 1 - Ground tests / 1
Y 3.N 21/5:11/E177 Investigation of ice formation in the induction system of an aircraft engine. : 2 - Flight tests / 1
Y 3.N 21/5:11/E178 The effect of liquid and ice particles on the erosion of a supercharger-inlet cover and diffuser vanes / 1
Y 3.N 21/5:11/E179 Relation between fuel economy and crank angle for the maximum rate of pressure rise / 1
Y 3.N 21/5:11/E18 A laboratory investigation of the icing characteristics of the Bendix-Stromberg carburetor model PD-12F5 with the Pratt and Whitney R-1830-C4 intermediate rear engine section / 1
Y 3.N 21/5:11/E180 The effect of six aromatic amines on the preignition-limited performance of 28-R aviation fuel in a CFR engine / 1
Y 3.N 21/5:11/E181 Process of lead-deposit accumulations on aircraft-engine spark plugs / 1
Y 3.N 21/5:11/E182 A laboratory-tested constant-level oil sump to prevent aeration of scavenged oil from an aircraft engine / 1
Y 3.N 21/5:11/E183 The effect of ethylene dibromide on the knock-limited performance of leaded and nonleaded S reference fuel / 1
Y 3.N 21/5:11/E184 Reduction of fuel-vapor loss by omitting some of the fuel constituents normally lost during flight / 1
Y 3.N 21/5:11/E185 Analysis and correlation of data obtained by six laboratories on fuel-vapor loss from fuel tanks during simulated flight / 1
Y 3.N 21/5:11/E186 Flight variables affecting fuel-vapor loss from a fuel tank / 1
Y 3.N 21/5:11/E187 Operating stresses in aircraft-engine crankshafts and connecting rods. : 1 - Slip-ring and brush combinations for dynamic-strain measurements / 1