Modeling and validation of the thermal effects on gas turbine transients

Journal of Engineering for Gas Turbines and Power

Volumn 127, Issue 3, 2005, Pages 564-572

  Nielsen, Annette E ^a   Moll, Christoph W ^b   Staudacher, Stephan ^c  

^a Rolls Royce Deutschland Ltd and CoKG ^*  (Germany)

^b ROLLS ROYCE DEUTSCHLAND LTD AND CO KG   (Germany)

^c UNIVERSITY OF STUTTGART   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CODES (STANDARDS); COMPUTER SIMULATION; HEAT TRANSFER; MATHEMATICAL MODELS; STATE SPACE METHODS; THERMAL EFFECTS;

ENGINE STRUCTURE; GAS TURBINE TRANSIENTS; STATE SPACE STRUCTURES;

GAS TURBINES;

GAS TURBINE;

EID: 22744434719     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1850495     Document Type: Article

References (8)

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3. Fiola, R., 1993, "Berechnung des Instationären Betriebsverhaltens unter Besonderer Berücksichtigung von Sekundäreffekten," Doctor thesis, Technical University of Munich.
4. Riegler, C., 1999, "Correlations to Include Heat Transfer in Gas Turbine Performance Calculations," Aerospace Science and Technology, No. 5, pp. 281-292.
5. Frank, R., Rist, D., and Kappler, G., 1993, "On-line Überwachung der Ermüdungslebensdauer von Rotierenden Flugtriebwerkskomponenten," DGLR Jahresbuch No. 93-03-048.
6. 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.
7. Staudacher, S., 1995, "Untersuchungen zum sekundären Luftsystem von Luftstrahltriebwerken," Doctor thesis, Technical University of Munich.
8. 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.