Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering
Reference19 articles.
1. Assessment of rich-burn, quick-mix, lean-burn trapped vortex combustor for stationary gas turbines;Straub;Journal of Engineering for Gas Turbines and Power,2005
2. S.K. Kim, T.V. Breikin, S.M. Hargrave, H.A. Thompson, P.J. Fleming, S.J. Riley, Staged combustion control for aviation engines: a multi-objective optimisation approach, 15th Triennial World Congress, 2002 IFAC, Barcelona, Spain.
3. C. Hassa, C.E. Migueis, P. Voigt, Design principles for the quench zone of rich-quench-lean combustors, in: RTO AVT Symposium on “Design Principles and Methods for Aircraft Gas Turbine Engines”, May 1998, Toulouse, France.
4. Investigation of two advanced cooling mixing concepts for a rich-quench lean combustor;Diers;Journal of Engineering for Gas Turbines and Power,2002
5. Combustion in swirling flows: a review;Syred;Combustion and Flame,1974
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