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- Wind-tunnel tests of single- and dual-rotating pusher propellers having from three to eight blades
- An investigation of aircraft heaters V : theory and use of heat meters for the measurement of rates of heat transfer which are independent of time
- Investigation of extreme leading-edge roughness on thick low-drag airfoils to indicate those critical to separation
- Investigation of flow through an intercooler set at various angles to the supply duct
- Flight measurements of the lateral control characteristics of an airplane equipped with a combination aileron-spoiler control system
- Flight measurements of the rudder control and sideslip characteristics of four vertical tail arrangements on the P-40 series airplanes
- Investigation of means for extending the range of several bombers to 6000 miles
- An investigation of aircraft heaters I : elementary heat transfer considerations in an airplane
- An investigation of aircraft heaters IV : measured and predicted performance of longitudinally finned tubes
- An investigation of aircraft heaters VII : thermal radiation from athermanous exhaust gases
- An investigation of aircraft heaters III : measured and predicted performance of double tube heat exchangers
- An investigation of aircraft heaters VI : heat transfer equations for the single pass longitudinal exchanger
- An investigation of aircraft heaters II : properties of gases
- Investigation of the variation of lift coefficient with Reynolds number at a moderate angle of attack on a low-drag airfoil
- Measurements of the flying qualities of a Supermarine Spitfire VA airplane
- A method for the design of cooling systems for aircraft power-plant installations
- Measurements of the flying qualities of a Hawker Hurricane airplane
- A method of calculating bending stresses due to torsion
- Normal-pressure tests of rectangular plates
- New method of extrapolation of the resistance of a model planing boat to full size
- Investigation of Diving Moments of a Pursuit Airplane in the Ames 16-Foot High Speed Wind Tunnel
- Preliminary investigation and design of an air-heated wing for Lockheed 12A airplane
- The preparation of 2, 2, 4, 4-tetramethylpentane
- Procedure used at Aluminum Research Laboratories for determining type of attack in some aluminum alloys
- Principles and methods of rating and testing centrifugal superchargers
- The mean aerodynamic chord and the aerodynamic center of a tapered wing
- Full-scale tunnel investigation of the control and stability of a twin-engine monoplane with propellers operating
- Full-scale-tunnel investigation of a multiengine pusher-propeller installation
- Identification of knock in NACA high-speed photographs of combustion in a spark-ignition engine
- Effect of countersunk depth on the tightness of two types of machine-countersunk rivet
- Bending of rectangular plates with large deflections
- Comparison of Intercooler Characteristics
- The effect of various surface conditions on press fits of steel bushings and 17S-T aluminum-alloy fittings
- The effect of propeller operation on the air flow in the region of the tail plane for a twin-engine tractor monoplane
- Summary report on the induction of water to the inlet air as a means of internal cooling in aircraft-engine cylinders
- The resistance coefficient of commercial round wire grids
- A study by high-speed photography of combustion and knock in a spark-ignition engine
- Statistical analysis of service stresses in aircraft wings
- Some theoretical considerations of longitudinal stability in power-on flight with special reference to wind-tunnel testing
- Thermal Theory of Combustion and Explosion
- Effect of additions of aromatics on the knocking characteristics of several 100-octane fuels at two engine speeds
- Aerodynamic problems in the design of efficient propellers
- An analysis of the effect of core structure and performance on volume and shape of cross-flow tubular intercoolers
- The fatigue strengths of some wrought aluminum alloys
- The cross-flow plate-type intercooler
- Effect of an aromatic mixture added to two 100-octane fuels on engine temperatures and fuel consumption
- Maximum permissible engine performance of eight representative fuels of 100-octane number
- Performance of two-stage turbosupercharger using mixed-flow impellers
- An investigation of diffuser-resistance combinations in duct systems
- Ground effect on downwash angles and wake location