In this paper, we present a methodology to integrated simulation of gas turbine engine (GTE). This method allow to predict performance of GTE components workflows with account the mutual influence. Steady state CFD modeling of compressor, combustion chamber and the turbine are demonstrated. Solution is provided in separate solvers step by step. Efforts to decide some problem of matching models are written. Author shows the accuracy level of boundary data achieved with this approach.
Account the Mutual Influence of the Simulation Components of GTE
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Krivcov, A, Shabliy, L, & Baturin, O. "Account the Mutual Influence of the Simulation Components of GTE." Proceedings of the ASME 2014 Gas Turbine India Conference. ASME 2014 Gas Turbine India Conference. New Delhi, India. December 15–17, 2014. V001T11A004. ASME. https://doi.org/10.1115/GTINDIA2014-8211
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