Abstract
Continuous improvement of efficiency and performance of aircraft and power generation gas turbine systems during the past decades has led to engine designs that are subject to extreme load conditions. Despite the enormous progress in the development of materials, at the design point, the engine components operate near their aerodynamic, thermal, and mechanical stress limits. Under these circumstances, any adverse dynamic operation causes excessive aerodynamic, thermal, and subsequent mechanical stresses that may affect the engine safety and reliability, and, thus, the operability of the engine if adequate precautionary actions are not taken.
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References
1. Koenig R.W., Fishbach L.H., 1972, “ GENENG- A Program for Calculating Design and Off-Design Performance for Turbojet and Turbofan Engines,” NASA TN D-6552.
2. Seldner K., Mihailowe J.R., Blaha R.J., 1972, “Generalized Simulation Technique for Turbojet Engine System Analysis,” NASA TN D-6610.
3. Szuch J.R., 1974, “HYDES- A Generalized Hybrid Computer Program for Studying Turbojet or Turbofan Engine Dynamics,” NASA TM X-3014.
4. Seller J., Daniele C.J., 1975, “DYGEN- A Program for Calculating Steady-State and Transient Performance of Turbojet and Turbofan Engines,” NASA TND-7901.
5. Schobeiri M.T., 1985 “Aero-Thermodynamics of Unsteady Flows in Gas Turbine Systems.” Brown Boveri Company, Gas Turbine Division Baden Switzerland, BBC-TCG-51.
6. Schobeiri T., 1985 “COTRAN, the Computer Code for Simulation of Unsteady Behavior of Gas Turbines.” Brown Boveri Company, Gas Turbine Division Baden Switzerland, BBC-TCG-53
7. Schobeiri, T., 1985 “Digital Computer Simulation of the Dynamic Response of Gas Turbines”, VDI- Annual Journal of Turbomachinery, pp. 381-400, 1985.
8. Schobeiri T., 1986: “A General Computational Method for Simulation and Prediction of Transient Behavior of Gas Turbines.” ASME-86-GT-180.
9. Schobeiri T., 1987, “Digital Computer Simulation of the Dynamic Operating Behavior of Gas Turbines.” Journal Brown Boveri Review 3-87.
10. Schobeiri T., 1987, “Digital Computer Simulation of the Dynamic Operating Behavior of Gas Turbines.” Journal Brown Boveri Review 3-87.
11. Schobeiri, H. Haselbacher, H, 1985c, “Transient Analysis of Gas Turbine Power Plants Using the Huntorf Compressed Air Storage Plant as an Example.” ASME-85-GT-197.
12. Schobeiri, M. T., Attia, M, Lippke, C., 1994, “Nonlinear Dynamic Simulation of Single and Multi-spool Core Engines, Part I: Theoretical Method,” AIAA, Journal of Propulsion and Power, Volume 10, Number 6, pp. 855-862, 1994.
13. Schobeiri, M. T., Attia, M, Lippke, C., 1994, “Nonlinear Dynamic Simulation of Single and Multi-spool Core Engines, Part II: Modeling and Simulation Cases,” AIAA Journal of Propulsion and Power, Volume 10, Number 6, pp. 863-867, 1994.
14. Schobeiri, M. T., 1982, “Dynamisches Verhalten der Luftspeichergasturbine Huntorf bei einem Lastabwurf mit Schnellabschaltung,” Brown Boveri, Technical Report, TA-58.
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Schobeiri, M.T. (2018). Simulation of Gas Turbine Engines, Design Off-Design and Dynamic Performance. In: Gas Turbine Design, Components and System Design Integration. Springer, Cham. https://doi.org/10.1007/978-3-319-58378-5_18
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DOI: https://doi.org/10.1007/978-3-319-58378-5_18
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