Abstract
A turbomachinery system such as a power generation gas turbine engine, a thrust generation aero- engine, rocket propulsion, or a small turbocharger, consist of several sub-systems that we call components ([1], [2], [3], [4]). Each component is an autonomous entity with a defined function within the system. Inlet nozzles, exit diffusers, combustion chambers, compressors, and turbines are a few component examples. A component may consist of several sub-components.
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References
1. Schobeiri, M. T., Abouelkheir, M., Lippke, C., 1994, “GETRAN: A Generic, Modularly Structured Computer Code for Simulation of Dynamic Behavior of Aero-and Power Generation Gas Turbine Engines,” an honor paper, ASME Transactions, Journal of Gas Turbine and Power, Vol. 1, pp. 483-494.
2. Schobeiri T., 1986: “A General Computational Method for Simulation and Prediction of Transient Behavior of Gas Turbines.” ASME-86-GT-180.
3. Schobeiri M. T., 1985 “Aero-Thermodynamics of Unsteady Flows in Gas Turbine Systems.” Brown Boveri Company, Gas Turbine Division Baden Switzerland, BBC-TCG-51.
4. Schobeiri M.T., 1985b “COTRAN, the Computer Code for Simulation of Unsteady Behavior of Gas Turbines.” Brown Boveri Company, Gas Turbine Division Baden Switzerland, BBC-TCG-53-Technical Report.
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Schobeiri, M.T. (2018). Generic Modeling of Turbomachinery Components and Systems. In: Gas Turbine Design, Components and System Design Integration. Springer, Cham. https://doi.org/10.1007/978-3-319-58378-5_12
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DOI: https://doi.org/10.1007/978-3-319-58378-5_12
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