Low-NOx combustors for hydrogen fueled aero engine

International Journal of Hydrogen Energy

Volumn 23, Issue 4, 1998, Pages 281-288

  Ziemann, J ^a   Shum, F ^b   Moore, M ^b   Kluyskens, D ^c   Thomaier, D ^a   Zarzalis, N ^a   Eberius, H ^d  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b PRATT AND WHITNEY CANADA   (Canada)

^c HYDRO QUÉBEC   (Canada)

^d GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; COMBUSTORS; COMPUTER SIMULATION; FUELS; HYDROGEN;

KINETIC MODELLING;

AIRCRAFT ENGINES;

EID: 0032036108     PISSN: 03603199     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0360-3199(97)00054-2     Document Type: Article

References (6)

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3. McVey, J. B., Padget, F. C., Rosfjord, T. J., Hu, A. S., Peracchio, A. A., Schlein, B. and Tegel, D. R., Evaluation of low NOx combustor concepts for aeroderivative gas turbine engines. ASME 92-GT-133, IGTACE, Cologne, June 1992.
4. Rosfjord, T. J. and Cohen, J. M., Evaluation of the transient operation of advanced gas turbine combustors, AIAA Journal of Propulsion and Power, 1995, 11(3), 497-504.
5. Anderson, J. D., Hypersonic and High Temperature Gas Dynamics. McGraw Hill, New York, 1989.
6. Miller, J. A. and Bowman, C. T., Mechanism and modelling of nitrogen chemistry in combustion progress, Energy Combustion Science, 1989, 15, 287-338.