Recent Progress in Comprehensive Modeling of Gas Turbine Combustion
Author:
Affiliation:
1. GE Aviation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1445
Reference156 articles.
1. Mongia, H. C., Reynolds, R. S., Coleman, E., and Bruce, T. W., 1979, "Combustor Design Criteria Validation Volume II - Development testing of two full-scale annular gas turbine combustors", USARTL-TR-78-55B (AD-AO-67689).
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