TECHNICAL PAPERS: Gas Turbines: Heat Transfer

Modeling and Validation of the Thermal Effects on Gas Turbine Transients

[+] Author and Article Information
Annette E. Nielsen

Hermann-Eckert-Strasse 20, D-88634 Herdwangen-Schoenach, Germanye-mail: annette.nielsen@rolls-royce.com

Christoph W. Moll

Rolls-Royce Deutschland Ltd., & CoKG, Eschenweg 15, 15827 Dahlewitz, Germanye-mail: christoph.moll@rolls-royce.com

Stephan Staudacher

Institut für Luftfahrtantriebe, University Stuttgart, Pfaffenwaldring 6, 70596 Stuttgart, Germanye-mail: staudacher@ila.uni-stuttgart.de

J. Eng. Gas Turbines Power 127(3), 564-572 (Jun 24, 2005) (9 pages) doi:10.1115/1.1850495 History: Received October 01, 2003; Revised March 01, 2004; Online June 24, 2005
Copyright © 2005 by ASME
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Therkorn, D., 1992, “Fortschrittliches Leistungs-Berechnungsverfahren für luftatmende Turbotriebwerke,” Doctor thesis, University of Stuttgart.
Khalid, S. J., and Hearne, R. E., 1980, “Enhancing Dynamic Model Fidelity for Improved Prediction of Turbofan Engine Transient Performance,” AIAA 80-1083.
Fiola, R., 1993, “Berechnung des Instationären Betriebsverhaltens unter Besonderer Berücksichtigung von Sekundäreffekten,” Doctor thesis, Technical University of Munich.
Riegler, C., 1999, “Correlations to Include Heat Transfer in Gas Turbine Performance Calculations,” Aerospace Science and Technology, No. 5, pp. 281–292.
Frank, R., Rist, D., and Kappler, G., 1993, “On-line Überwachung der Ermüdungslebensdauer von Rotierenden Flugtriebwerkskomponenten,” DGLR Jahresbuch No. 93-03-048.
Peters, P., Breisig, V., Giboni, A., Lerner, C., and Pfost, H., 2000, “The Influence of the Clearance of Shrouded Rotor Blade on the Development of the Flowfield and Losses in the Subsequent Stator,” ASME GT-478.
Staudacher, S., 1995, “Untersuchungen zum sekundären Luftsystem von Luftstrahltriebwerken,” Doctor thesis, Technical University of Munich.
Staudacher, S., Berns, W., and Ye, Haiwen, “Modeling Multistage Compressors by Several Split Compressors,” Institute for Aircraft Propulsion, University of Stuttgart, ALSTOM, Switzerland, AIAA 2003-1019.


Grahic Jump Location
Graphical representation of a state space system using a G matrix
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Quasi-non-linear state space model using integrated D,G, and C matrices
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Geometry and tip clearance definition
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Predicted HPC rotor 10 displacements and FE model
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Stagewise tip clearance changes HPT rotors
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Averaged tip clearance change HPC rotors
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Secondary processes and their effects in gas turbines
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Flow of nonadiabatic cycle matching
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Simulated and measured TGT overshoot
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Simulated and measured fuel flow overshoot
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Predicted and measured surge margin change
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Predicted and measured HPT pressure ratio




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