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Information Journal Paper

Title

THERMODYNAMIC DESIGN OF A POWER TURBINE FOR USING IN CONVERSION PROCESS OF A TURBOJET ENGINE TO A TURBO-SHAFT ENGINE

Pages

  27-39

Abstract

 In this paper, thermodynamic design of an axial flow POWER TURBINE for converting an existing turbojet to a turbo-shaft engine is presented. The exhaust nozzle of the turbojet is replaced by an axial flow POWER TURBINE. The turbine model is developed, based on Ainley-Mathieson model. The results of Ainley-Mathieson model were verified, using a 3D simulation and existing experimental data. The turbine performance was investigated for several blade angles of attack. Results show that the turbine stage has a minimum loss and a maximum efficiency, when angles of attack are -3 degrees for stator and -8 degrees for rotor blades.

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    APA: Copy

    SEDDIGHI, M., & FAZELI, H.. (2014). THERMODYNAMIC DESIGN OF A POWER TURBINE FOR USING IN CONVERSION PROCESS OF A TURBOJET ENGINE TO A TURBO-SHAFT ENGINE. FLUID MECHANICS AND AERODYNAMICS JOURNAL, 3(1 (11)), 27-39. SID. https://sid.ir/paper/245537/en

    Vancouver: Copy

    SEDDIGHI M., FAZELI H.. THERMODYNAMIC DESIGN OF A POWER TURBINE FOR USING IN CONVERSION PROCESS OF A TURBOJET ENGINE TO A TURBO-SHAFT ENGINE. FLUID MECHANICS AND AERODYNAMICS JOURNAL[Internet]. 2014;3(1 (11)):27-39. Available from: https://sid.ir/paper/245537/en

    IEEE: Copy

    M. SEDDIGHI, and H. FAZELI, “THERMODYNAMIC DESIGN OF A POWER TURBINE FOR USING IN CONVERSION PROCESS OF A TURBOJET ENGINE TO A TURBO-SHAFT ENGINE,” FLUID MECHANICS AND AERODYNAMICS JOURNAL, vol. 3, no. 1 (11), pp. 27–39, 2014, [Online]. Available: https://sid.ir/paper/245537/en

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