Call Number (LC) Title Results
Y 3.N 21/5:11/W-19 An investigation of aircraft heaters. : XV - The emissivity of several materials / 1
Y 3.N 21/5:11/W-20 An investigation of aircraft heaters. : IX - Measured and predicted performance of two exhaust gas-air heat exchangers and an apparatus for evaluating exhaust gas-air heat exchangers / 1
Y 3.N 21/5:11/W-21 An investigation of aircraft heaters. : XIV - An air and heat flow analysis of a ram-operated heater and duct system / 1
Y 3.N 21/5:11/W-22 An investigation of aircraft heaters. : XVI - Determination of the viscosity of exhaust gases from a gasoline engine / 1
Y 3.N 21/5:11/W-23 An investigation of aircraft heaters. : I - Elementary heat transfer considerations in an airplane / 1
Y 3.N 21/5:11/W-24 An investigation of aircraft heaters. : XVII - Experimental inquiry into steady state unidirectional heat-meter corrections / 1
Y 3.N 21/5:11/W-25 An investigation of aircraft heaters. : XIX - Performance of two finned-type crossflow exhaust gas and air heat exchangers / 1
Y 3.N 21/5:11/W-26 An investigation of aircraft heaters. : XXII - Measured and predicted performance of a fluted-type exhaust gas and air heat exchanger / 1
Y 3.N 21/5:11/W-27 An investigation of aircraft heaters. : XXI - Measured and predicted performance of a flattened-tube type crossflow exhaust gas and air heat exchanger / 1
Y 3.N 21/5:11/W-28 An investigation of aircraft heaters. : XX - Measured and predicted performance of a finned-type cast-aluminum crossflow exhaust gas and air heat exchanger / 1
Y 3.N 21/5:11/W-29 An investigation of aircraft heaters. : XXIII - Measured and predicted performance of a flat-plate type exhaust gas and air heat exchanger / 1
Y 3.N 21/5:11/W-30 An investigation of aircraft heaters. : XXIV - The heat meter in the transient state for unidirectional heat transfer / 1
Y3.N 21/5:11/W-32 The significance of the time concept in engine detonation / 1
Y 3.N 21/5:11/W-33 A method of shear-lag analysis of box beams for axial stresses, shear stresses, and shear center / 1
Y 3.N 21/5:11/W-34 Procedure used at Aluminum Research Laboratories for determining type of attack in some aluminum alloys / 1
Y 3.N 21/5:11/W-36 The problem of thermal-expansion stresses in reinforced plastics / 1
Y 3.N 21/5:11/W-37 A method for studying piston friction / 1
Y 3.N 21/5:11/W-38 Progress report on fatigue of spot-welded aluminum / 1
Y 3.N 21/5:11/W-39 Pressure loss in ducts with compound elbows / 1
Y 3.N 21/5:11/W-40 Altitude rating of electrical apparatus / 1