Performance of two air-cooled turbojet engines determined analytically from engine component performance for a range of cooling-air weight flows
Description: Report presenting an analysis of two turbojet engines, including the component performance of the compressors and turbines, in order to determine the effect on engine performance and operation of bleeding the compressor to furnish cooling air for the turbine rotor blades. Results regarding the compressor and turbine performance characteristics and engine performance characteristics are provided.
Date: February 18, 1954
Creator: Ziemer, Robert R.; Schafer, Louis J., Jr. & Heaton, Thomas R.
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Partner: UNT Libraries Government Documents Department