| [1] 陈懋章, 刘宝杰. 大涵道比涡扇发动机风扇/压气机气动设计技术分析[J]. 航空学报, 2008, 29(3): 513-526. CHEN M Z, LIU B J. Fan/compressor aero design technology for high bypass radio turbofan[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(3): 513-526 (in Chinese).
[2] 陈懋章. 风扇/压气机技术发展和对今后工作的建议[J]. 航空动力学报, 2002, 17(1): 1-15. CHEN M Z. Development of fan/compressor techniques and suggestions on further researches[J]. Journal of Aerospace Power, 2002, 17(1): 1-15 (in Chinese).
[3] 陈光. 波音787用发动机设计特点[M]. 北京: 北京航空航天大学出版社, 2007. CHEN G. Design characteristics of engine for B787[M]. Beijing: Beihang University Press, 2007 (in Chinese).
[4] 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. 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).
[5] RITI S. Fifty years of civil aero gas turbines[J]. Aircraft Engineering and Aerospace Technology, 1996, 68(4): 3-19.
[6] 航空发动机设计手册总编委会. 航空发动机设计手册: 第8册[M]. 北京: 航空工业出版社, 2000. The Editorial Committee of Aero-engine Design Manual. Aero-engine design manual: Volume 8[M]. Beijing: Aviation Industry Press, 2000 (in Chinese).
[7] 冀国锋, 桂幸民. 轴流/离心压气机通用任意中弧造型设计方法研究[J]. 航空动力学报, 2009, 24(1): 150-156. JI G F, GUI X M. A blading design method for axial/centrifugal compressor airfoils using arbitrary camber lines[J]. Journal of Aerospace Power, 2009, 24(1): 150-156 (in Chinese).
[8] 陈懋章. 叶轮机气动力学研究现状及其发展趋势[C]//第五届动力年会论文集. 北京: 中国航空学会, 2003. CHEN M Z. Present status and future development of the studies for turbomachinery aerodynamics[C]//Proceedings of the 5th Power Annual Conference. Beijing: Chinese Society of Aeronautics and Astronautics, 2003 (in Chinese).
[9] 梁春华. 高性能航空发动机先进风扇和压气机叶片综述[J]. 航空发动机, 2006, 32(3): 48-52. LIANG C H. Overview of advanced fan and compressor blade/vane in high performance aeroengine[J]. Aeroengine, 2006, 32(3): 48-52 (in Chinese).
[10] 程荣辉. 轴流压气机设计技术的发展[J]. 燃气涡轮试验与研究, 2004, 17(2): 1-8. CHENG R H. Development technology for axial compressor[J]. Gas Turbine Experiment and Research, 2004, 17(2): 1-8 (in Chinese).
[11] 靳允立, 胡骏. 叶片弯掠对多级风扇气动性能的影响[J]. 推进技术, 2009, 30(1): 77-83. JIN Y L, HU J. Effects of swept-curved blade on the performance of the multistage[J]. Journal of Propulsion Technology, 2009, 30(1): 77-83 (in Chinese).
[12] 朱芳, 陈云永, 卫飞飞, 等. 某民用大涵道比涡扇发动机风扇缩尺试验件气动性能数值仿真[J]. 航空动力学报, 2013, 28(7): 1539-1548. ZHU F, CHEN Y Y, WEI F F, et al. Numerical simulation of aerodynamic performance of scaled fan of a civil high-bypass-ration turbo engine[J]. Journal of Aerospace Power, 2013, 28(7): 1539-1548 (in Chinese).
[13] 刘宝杰, 邹正平, 严明. 叶轮机计算流体动力学技术现状及其发展趋势[J]. 航空学报, 2002, 23(5): 394-404. LIU B J, ZOU Z P, YAN M. Present status and future development of CFD in turbomachinery[J]. Acta Aeronautic et Astronautica Sinica, 2002, 23(5): 394-404 (in Chinese).
[14] 乔渭阳. 航空发动机气动声学[M]. 北京: 北京航空航天大学出版社, 2010. QIAO W Y. Aero acoustics of aircraft engine[M]. Beijing: Beihang University Press, 2010 (in Chinese).
[15] MCALPINE A, FISHER J. On the prediction of buzz-saw noise generated by an aeroengine: AIAA-2000-2095[R]. Reston, VA: AIAA, 2000.
[16] MCALPINE A, FISHER J. On the prediction of "buzz-saw" noise in aero-engine inlet ducts[J]. Journal of Sound and Vibration, 2001, 248(1): 123-149.
[17] 王晓宇. 传递单元方法及其在航空发动机短舱声学问题中的应用[D]. 北京: 北京航空航天大学, 2010. WANG X Y. Transfer element method and the applications on the nacelle of aircraft engine[D]. Beijing: Beihang University, 2010 (in Chinese).
[18] SCHULTEN J B H M. Vane sweep effects on rotor/stator interaction noise[J]. AIAA Journal, 1997, 35(6): 945-951.
[19] LOWSON M V. Reduction of compressor noise radiation[J]. Journal of the Acoustical Society of America, 1968, 43(1): 37-50.
[20] 李杰. GE公司复合材料风扇叶片的发展和工艺[J]. 航空发动机, 2008, 34(4): 54-55. LI J. Development and technology for complex material fan blade of GE[J]. Aeroengine, 2008,34(4): 54-55 (in Chinese). |
CJA
