Effect of heat and power extraction on turbojet-engine performance I : analytical method of performance evaluation with compressor-outlet air bleed
Reece V. Hensley, F. E. Rom, S.L. Koutz
Abstract
Reece V. Hensley, F. E. Rom, S.L. Koutz
Abstract
Report presenting an analytical investigation of the performance of a turbojet engine with air bled off at the compressor outlet. A wide range of engine and flight conditions are covered and air bleeds of 0 to 15 percent of the air mass flow are considered. Results are provided in the form of generalized performance charts that are applicable to a wide range of operating conditions.
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Report presenting an analytical investigation of the performance of a turbojet engine with air bled off at the compressor outlet. A wide range of engine and flight conditions are covered and air bleeds of 0 to 15 percent of the air mass flow are considered. Results are provided in the form of generalized performance charts that are applicable to a wide range of operating conditions.
Key concepts: Turbojet, Gas compressor, Range (aeronautics), Engineering, Automotive engineering, Bleed, Engine power, Mass flow