The Effect of Fuel Composition, Compression Pressure, and Fuel-air Ratio on the Compression-ignition Characteristics of Several Fuels
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Kinetics in hydrogen air flow systems - calculation of autoignition delays for hypersonic ramjets
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Presents an analysis of a compound engine operating with manifold pressures ranging from 60 to 110 lb/sq in. absolute. The effects of engine limits (peak cylinder pressure and turbine-inlet temperature) and component efficiency are discussed. A range analysis is used to evaluate the merit of the engine. The analysis indicates that specific-fuel-consumption values of 0.32 lb/bhp-hr and specific weights of 0.8 lb/bhp are obtainable at high manifold pressures.
This report examines the cause and effect of the energy conversion in airless-injection engines. In order to obtain a criterion for the chosen working method, it takes into consideration the time relations between the individual processes. Observations of the engine alone do not suffice to obtain the necessary basis for a critical analysis of the processes.
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Effect of grid and constriction friction on flame propagation velocity, heat exchange and acoustic shock discontinuity formation in reactive media
Combustion analysis of hydrogen, oxygen and nitrogen dioxide mixtures
Low cost, ambient temperature catalyst for reacting hydrogen gas with air in a catalytic cell near the point of evolution at a controlled rate is announced.
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrate