[1] Gliebe P R, Janardan B A. Ultra-high bypass engine aeroacoustic study, NASA/CR-2003-212525. Washington, D.C.: NASA, 2003.[2] Pierret S, Kato H, Coelho R F, et al. Aero-mechanical optimization method with direct CAD access-application to counter rotating fan design, ASME Paper, GT-2006-90505. New York: ASME, 2006.[3] Ji L C. Analysis of technical challenges in vaneless counter-rotating turbomachinery, ASME Paper, GT-2007-27617. New York: ASME, 2007.[4] Lynam F C, Hawes S P. Contra rotating axial flow fans[J]. The Engineers, 1946: 1-8.[5] Young R H. Contra-rotating axial-flow fans[J]. Journal of Institute Heating Ventilating Engineering, 1951, 18: 448-477.[6] Sabel S, Sabatuik S. Turbojet engine development design of phase I & II compressor, Currtise Wright Cooperation(CWR), Report No. 502a and 502b. 1957.[7] Millar D A J, Chappel M S, Okelah R. The co-turbo shaft-A novel gas turbine power plant for heavy equipment, ASME Paper, GT-79-132. New York: ASME, 1979.[8] Newton A G. Aero gas turbine engines for commercial application//7th International Symposium on Air Breathing Engines, 1985.[9] Baldeo M K. Unducted fan engines[J]. Boeing Airliner Magazine (USA), 1987(1-3): 1-15.[10] Sharma P B, Adekoya A. A review of recent research on contra-rotating axial flow compressor stage, ASME Paper, GT-96-254. New York: ASME, 1996.[11] Sharma P B, Jain Y P, Jha N K, et al. Stalling behavior of a contra-rotating stage//7th International Symposium on Air Breathing Engines, 1985: 734-740.[12] Sharma P B, Jain Y P, Pundhir D S. A study of some factors affecting the performance of a contra-rotating axial compressor stage[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 1988, 202(1): 15-21.[13] Kerrebrock J L, Epstein A H, Merchant A A, et al. Design and test of an aspirated counter-rotating fan, ASME Paper, GT-2006-90582. New York: ASME, 2006.[14] Lengyel T, Vo C, Schmidt T, et al. Design of a counter rotating fan-An aircraft engine technology to reduce noise and CO2-emissions, ISABE-2009-1267. Cincinnati: ISABE, 2009.[15] Chen M Z, Liu B J. Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan[J]. Journal of Aerospace Power, 2008, 23(6): 961-975. (in Chinese) 陈懋章, 刘宝杰. 风扇/压气机气动设计技术发展趋势——用于大型客机的大涵道比涡扇发动机[J].航空动力学报,2008, 23(6): 961-975.[16] Saida J F, Dunba L W, Sizuks P N, et al. Counter rotating aeroengine with high total pressure ratio compressor: China, ZL03106813.8. 2003-03-03. (in Chinese) Saida J F, Dunba L W, Sizuks P N, 等.具有高总压比的压气机的反向旋转的航空燃气轮机: 中国, ZL03106813.8. 2003-03-03.[17] Wang Y G, Liu B, Chen Y Y, et al. Flow field investigation dual stage counter-rotating compressor[J]. Journal of Northwestern Polytechnical University, 2006, 24(1): 97-101. (in Chinese) 王掩刚, 刘波, 陈云永, 等.双级对转压气机流场分析[J]. 西北工业大学学报, 2006, 24(1): 97-101.[18] Liu B, Yang Y, Wang Y G, et al. Investigation of influence of rotational speed and pressure ratio on performance of two-stage counter-rotating compressor[J]. Journal of Northwestern Polytechnical University, 2007, 25(4):576-580. (in Chinese) 刘波, 杨艳, 王掩刚, 等. 设计压比和转速变化对对转压气机性能的影响研究[J]. 西北工业大学学报, 2007, 25(4): 576-580.[19] Yang L X, Zhao X L. Design and numerical investigation of a high-pressure ratio counter-rotating fan, ISABE-2007-1139. Cincinnati: ISABE, 2007.[20] Yang X H, Shan P. Aerodynamic design and investigation of two counter-rotating fans[J]. Journal of Aerospace Power, 2011, 26(10): 2313-2322. (in Chinese) 杨小贺, 单鹏. 两类对转风扇的设计与气动特征数值研究[J]. 航空动力学报, 2011, 26(10): 2313-2322.[21] Guo J, Yang L, Zhen N, et al. Investigation of critical technology for lift fan[J]. Aeronautical Science and Technology, 2008(2): 30-35.(in Chinese) 郭捷, 杨琳, 郑宁, 等. 短距/垂直起落战斗机升力风扇关键技术的探讨[J]. 航空科学技术, 2008(2): 30-35. |