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Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis

Description: A method of predicting equilibrium operating performance of turbojet engines has been developed, with the assumption of simple model processes for the components. Results of the analysis are plotted in terms of dimensionless parameters comprising critical engine dimensions and over-all operating variables. This investigation was made of an engine in which the ratio of axial inlet-air velocity to compressor-tip velocity is constant, which approximates turbojet engines with axial-flow compressors. Experimental correlation of the theory with data from several existing axial-flow-type engines was good and showed close correlation between calculated and measured performance.
Date: January 1, 1950
Creator: Sanders, John C & Chapin, Edward C
Partner: UNT Libraries Government Documents Department