Combustion instability investigations on the BR710 jet engine

Journal of Engineering for Gas Turbines and Power

Volumn 120, Issue 1, 1998, Pages 34-40

  Konrad, W ^a   Brehm, N ^a   Kameier, F ^b   Freeman, C ^c   Day, I J ^d  

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

^b Rolls Royce Deutschland Ltd Co KG   (Germany)

^c ROLLS ROYCE PLC   (United Kingdom)

^d UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0013328264     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2818085     Document Type: Article

References (8)

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2. Crocco, L., and Cheng, S. L., 1956, Theory of Combustion Instability in Liquid Propellant Rocket Motors, AGARDograph 8, Butterworths.
3. Culick, F., Heitor, M. V., and Whitelaw, J. H., 1996, Unsteady Combustion, NATO ASI Series, Serie E: Applied Sciences 306.
4. Hermann, J., Zangl, P., Gleis, S., and Vortmeyer, D., 1995, Untersuchung der Anregungsmechanismen selbsterregter Verbrennungsschwingungen an einem Verbrennungssystem fur Fliissigkraftstoff, VDI Berichte No. 1193, Deutsche!'Flammentag.
5. Kenworthy, M. J., Bahr, D., Mungur, P., Burrus, D. L., and Mehta, J. M, 1988, Dynamic Instability Characteristics of Aircraft Turbine Engine Comhustors, AGARD CP-450.
6. Lefebvre, A. H., 1983, Gas Turbine Combustion, McGraw-Hill, New York.
7. Putnam, A. A., 1971, Combustion-Driven Oscillations in Industry, Elsevier, New York.
8. Rayleigh, J., 1878, The Explanation of Certain Acoustical Phenomena, Nature, July 18, pp. 319-321.