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Steady-State Modelling of a Turbine Engine with Controllers

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Part of the book series: ISNM International Series of Numerical Mathematics ((ISNM,volume 115))

Abstract

Computer models of the behavior of a gas turbine engine coupled with a propeller are invaluable tools for engine design (Ping Zhu and Saravanamuttoo (1992), Rick and Muggli (1989)). Based on physical laws of mechanics and thermodynamics, and on experimentally given or computed characteristics of engine components, a mathematical description of the engine -propeller couple was proposed. It consist of a system of algebraic and differential equations. In Doležal et al. (1990, 1992) we described an implementation of the model of a moderately sized stand-alone gas turbine engine. The correspondence of computed results with measurements of real system was quite satisfactory.

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References

  • Bartholomew-Biggs M. C. (1990): A globally convergent version of REQP for constrained minimization. IMA J. Numer. Anal. 8, 253-271.

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  • Doležal J., Schindler Z., Fidler J., Matoušek O. (1992): Optimization-based decision support system for turbine power units modelling and design. Optimization-Based Computer-Aided Modelling and Design, Beulens A. J.M., Sebastian H.-J. (eds.), Lecture Notes in Control and Computer Science 174, Springer-Verlag, Berlin, 28-37.

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  • Ping Zhu, Saravanamuttoo H.I.H. (1992): Simulation of an advanced twin spool industrial gas turbine. Transactions of the ASME, J. of Engineering for Gas Turbines and Power, 114, No. 2, 180-186.

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© 1994 Birkhäuser Verlag Basel

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Schindler, Z. (1994). Steady-State Modelling of a Turbine Engine with Controllers. In: Bulirsch, R., Kraft, D. (eds) Computational Optimal Control. ISNM International Series of Numerical Mathematics, vol 115. Birkhäuser Basel. https://doi.org/10.1007/978-3-0348-8497-6_28

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  • DOI: https://doi.org/10.1007/978-3-0348-8497-6_28

  • Publisher Name: Birkhäuser Basel

  • Print ISBN: 978-3-7643-5015-4

  • Online ISBN: 978-3-0348-8497-6

  • eBook Packages: Springer Book Archive

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