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      Real-Time Gas Turbine Model for Performance Simulations

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          Abstract

          ABSTRACT Industry and universities around the world invest time and money to develop digital computer programs to predict gas turbine performance. This study aims to demonstrate a brand new digital model developed with the ability to simulate gas turbine real time high fidelity performance. The model herein described run faster than 30ms per point, which is compatible with a high-definition video refresh rate: 30 frames per second. This user-friendly model, built in Visual Basic in modular structure, can be easily configured to simulate almost all the existing gas turbine architectures (single, 2 or 3 shaft engines mixed or unmixed flows). In addition, its real time capability enables simulations with the pilot in the loop at earlier design phases when their feedback may lead to design changes for improvements or corrections. In this paper, besides the model description, it is presented the model run time capability as well as a comparison of the simulated performance with a commercial gas turbine tool for single, 2 and 3 shaft engine architecture.

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          Most cited references26

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          A Class of Methods for Solving Nonlinear Simultaneous Equations

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            Adaptive Simulation of Gas Turbine Performance

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              Tension des vapeurs: nouvelle relation entre les tension et les temperatures

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                Author and article information

                Contributors
                Role: ND
                Role: ND
                Role: ND
                Role: ND
                Journal
                jatm
                Journal of Aerospace Technology and Management
                J. Aerosp. Technol. Manag.
                Departamento de Ciência e Tecnologia Aeroespacial (São José dos Campos, SP, Brazil )
                1984-9648
                2175-9146
                September 2017
                : 9
                : 3
                : 346-356
                Affiliations
                [2] São José dos Campos São Paulo orgnameInstituto Tecnológico de Aeronáutica orgdiv1Departamento de Ciência e Tecnologia Aeroespacial orgdiv2Divisão de Engenharia Aeronáutica e Mecânica Brazil
                [1] São José dos Campos São Paulo orgnameEmpresa Brasileira de Aeronáutica Brazil
                Article
                S2175-91462017000300346
                10.5028/jatm.v9i3.693
                86a74439-4231-45c6-8fda-a41160ba558f

                This work is licensed under a Creative Commons Attribution 4.0 International License.

                History
                : 19 May 2016
                : 08 November 2016
                Page count
                Figures: 0, Tables: 0, Equations: 0, References: 26, Pages: 11
                Product

                SciELO Brazil


                Computer simulation,Propulsion,Gas turbines,Aircraft engines,Performance

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