Preliminary Tests in an Air-cooled Cylinder
Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel
Lead Susceptibility of Several Fuels as Determined in an Air-cooled Aircraft-engine Cyöinder
Analytical Determination of Effects of Shaft-power Extraction
Relative Effect of Cylinder-head and Inlet-mixture Temperatures Upon Knock Limits of Fuels
Theoretical Analysis of the Performance of a Supersonic Ducted Rocket
NACA Wartime Reports. Series E.
Mollier Diagrams for Air Saturated with Water Vapor at Low Temperatures
NACA Wartime Reports. Series L.
Analytical Method of Performance Evaluation with Compressor-outlet Air Bleed
Experimental Studies of the Knock-limited Blending Characteristics of Aviation Fuels
Knock-limited Blending Characteristics of Benzene, Toluene, Mixed Xylenes, and Cumene in an Air-cooled Cylinder
NACA Wartime Reports. Series E.
Theoretical Augmentation of Turbine-propeller Engine by Compressor-inlet Water Injection, Tail-pipe Burning, and Their Combination
Effect of Heat and Power Extraction on Turbojet-engine Performance
Theoretical Performance of an Axial-flow Compressor in a Gas-turbine Engine Operating with Inlet Water Injection
Loitering and Range Performance of Turbojet-powered Aircraft Determined by Off-design Engine Cycle Analysis
Effect of Heat and Power Extraction on Turbojet-engine Performance
Investigation of the I-40 Jet-propulsion Engine in the Cleveland Altitude Wind Tunnel