[1] MONGIA H K.Recent Advances in the Development of Combustor Design Tools[R].American Institute of Aeronautics and Astronautics,AIAA 2003-4495,2003:1-15.[2] CLINE M C,DEUR J M,MICKLOW G J,et al.Computation of the Flow Field in an Annular Gas Turbine Combustor[R].American Institute of Aeronautics and Astronautics,AIAA1993-2074,1993:1-25.[3] DANIAU E,BOUCHEZ M,BOUNACEUR R,et al.Contribution to Scramjet Active Cooling Analysis Using n-Dodecane Decompostion Model as a Generic Endothermic Fuel[R].International Society of Airbreathing Engines,ISABE-2001-1089,2001:1-16.[4] SIVARMAKRISHNA G.Combustor Geometry Optimization Studies Using CFD Techniques[R].International Society of Airbreathing Engines,ISABE-1998-114,1998:319-335.[5] JAMES E,BROAD WELL.A Turbulent Jet Chemical Reaction Model:NOx Production in Jet Flames Combustion and Flame[R].American Institute of Aeronautics and Astronautics,AIAA 2004-4198,2004:1-15.[6] DAGGETT,DAVID L,FUCKE,et al.Water Injection on Commercial Aircraft to Reduce Airport NO(x)[R].American Institute of Aeronautics and Astronautics,AIAA2002-3769,2002:1-20.[7] TURNER M G,RYDER R,NORRIS A,et al.High Fidelity 3D Turbofan Engine Simulation with Emphasis on Turbomanchinery Combustor Coupling[R].American Institute of Aeronautics and Astronautics,AIAA1998-3528,1998:1-25.[8] ZELINA J,CARDENA M,TOMONDI C,et al.Low-Emissions Gas Turbine Combustor Development Using Sector and Full Annular Rigs[R].American Institute of Aeronautics and Astronautics,AIAA1994-2768,1994:1-20.[9] FULLER E J,SMITH C E.CFD Analysis of a Research Gas Turbine Combustor Primary Zone[R].American Institute of Aeronautics and Astronautics,AIAA 99-2217,1999:1-20.[10] SURROGATE.Mixtures to Represent Complex Aviation and Rocket Fuel[R].American Institute of Aeronautics and Astronautics,A IAA 2003-6920,2003:1-18.[11] 罗景锋,刘小锋,高亚奎.飞机替代燃料研究综述[J].国际航空,2007(12):48-49.[12] 范学军,俞刚.大庆RP-3航空煤油热物性分析[J].推进技术,2006,27(2):187-191.[13] 李锋,孙佰刚,彭浪青,等.发动机双环腔燃烧室设计及性能分析[J].航空科学技术,2008(2):17-21.[14] 殷建平.中国燃料乙醇发展潜力分析[J].中国石油大学学报,2007,23(6):6-9.[15] 刘发发,谷艳华.乙醇均质压燃燃烧的化学反应动力学模型[J].吉林大学学报,2009,39(1):21-26.[16] 李锋,尚守堂,程明,等.双环腔燃烧室置换单环腔燃烧室可行性研究[J].航空动力学报,2008,23(1):145-149. |