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• An investigation of aircraft heaters XXIII : measured and predicted performance of a flat-plate type exhaust gas and air heat exchanger
• An investigation of aircraft heaters XXII : measured and predicted performance of a fluted-type exhaust gas and air heat exchanger
• Improving engine cooling with special baffles
• Suitability of ethers as aviation fuel components the knock-limited performance of several ethers blended with AN-F-28 fuel
• Method of Matching Performance of Compressor Systems with that of Aircraft Power Sections
• Performance effect of fully shrouding a centrifugal supercharger impeller
• Performance comparison of two deep inducers as separate components and in combination with an impeller
• Calculations of the Performance of a Compression-Ignition Engine-Compressor Turbine Combination I : Performance of a Highly Supercharged Compression-Ignition Engine
• The Effect of Inlet Temperature and Pressure on the Efficiency of Single-Stage Impulse Turbine Having a 13.2-Inch Pitch-Line Diameter Wheel
• Air-flow and performance characteristics of the engine-stage supercharger of a double-row radial aircraft engine I: effect of operating variables
• The knock-limited performance of fuel blends containing aromatics 4: data for m-diethylbenzene, 1-ethyl-4-methylbenzene and sec-butylbenzene together with a summarization of data for 12 aromatic hydrocarbons
• The knock-limited performance of fuel blends containing aromatics Part II : isopropylbenzene, benzene, and o-xylene
• A method for determining the rate of heat transfer from a wing or streamline body
• The knock-limited performance of fuel blends containing aromatics Part 3: 1,3,5-trimethylbenzene, tert-butylbenzene and 1,2,4-trimethylbenzene
• A visual photographic study of cylinder lubrication
• An investigation of backflow phenomenon in centrifugal compressors
• A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane
• Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder
• Application of a numerical procedure to stress analysis of stringer-reinforced panels
• The application of data on strength under repeated stresses to the design of aircraft
• A theoretical analysis of the performance of a diesel engine-compressor-turbine combination for aircraft
• Efficiency tests of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with air as the driving fluid
• An Experimental Investigation of NACA Submerged-Duct Entrances
• The Performance of a Single-Stage Impulse Turbine Having an 11.0-Inch Pitch-Line Diameter Wheel with Cast Airfoil-Shaped and Bent Sheet-Metal Nozzle Blades
• The effects of an increase in the concentration of ethylene dibromide in a leaded fuel on lead deposition, corrosion of exhaust valves, and knock-limited power
• Test of 0.14-scale models of the control surfaces of Army Project MX-511 in attitudes simulating spins
• A general representation for axial-flow fans and turbines
• The effect of two inlet-duct designs on turbine efficiency
• Measurements of recovery factors and coefficients of heat transfer in a tube for subsonic flow of air
• Friction in pipes at supersonic and subsonic velocities
• Bonding strengths of adhesives at normal and low temperatures
• Summary of Airfoil Data
• The inward bulge type buckling of monocoque cylinders III : revised theory which considers the shear strain energy
• Stresses in and general instability of monocoque cylinders with cutouts II : calculation of the stresses in a cylinder with a symmetric cutout
• An investigation of a thermal ice-prevention system for a C-46 cargo airplane VI : dry-air performance of thermal system at several twin- and single-engine operating conditions at various altitudes
• An investigation of a thermal ice-prevention system for a C-46 cargo airplane V : effect of thermal system on airplane cruise performance
• Correlation of exhaust-valve temperatures with engine operating conditions and valve design
• An experimental investigation of rectangular exhaust-gas ejectors applicable for engine cooling
• Ultraviolet spectrochemical analysis for aromatics in aircraft fuels
• A general representation for axial-flow fans and turbines
• Table of Interplanar Spacings for Crystal-Structure Determinations by X-Ray Diffraction With Molybdenum, Copper, Cobalt, Iron, and Chromium Radiations
• Flight Investigation of Boundary-Layer Transition and Profile Drag of an Experimental Low-Drag Wing Installed on a Figher-Type Airplane
• Shear Elastic Properties of Some High Strength Nonferrous Metals as Affected by Plastic Deformation and by Heat Treatment
• Effect of Aging Aircraft Structures on Magnesium Parts
• Force and Moment Coefficients for a Thin Airfoil With Flap and Tab in a Form Useful for Stability and Control Calculations
• The Strength of Semielliptical Cylinders Subjected to Combined Loadings
• A Photoelectric Hygrometer
• Strength of Wing Beams Under Axial and Transverse Loads
• Column Strength of Extruded Magnesium Alloys AM-C58S and AM-C58S-T5
• Protection of Nonmetallic Aircraft From Lightning 4: Electrocution Hazards From Inductive Voltages