Abstract
The paper describes the concept of modeling the turbine engine axial-flow compressor and turbine characteristics by using the function of two variables. Accuracy of the proposed concept has been verified on the example of the given compressor and turbine characteristics. Good agreement between the modeling results and experimental characteristics has been achived.References
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I.H. ISMAIL and F.S. BHINDER, Simulation of aircraft gas turbine engine, J. Engng. for Gas Turbines and Power, Transactions of the ASME, Vol. 113, New York 1991, pp.
95-99.
M.A. EL-GAMMAL, An algorithm and criteria for compressor characteristics real time modeling and approximation, J .Engng. for Gas Turbines and Power, Transactions of the ASME, Vol. 113, New York 1991, pp. 112-117.
J. HORMOUZIADIS and H. HERBIG, Numerische Simulation der Kennfelder von Strömungsmaschinen, Konstruktion, pp. 182-186, 26, 1974.
