| [1] Whitcomb R T. Review of NASA supercritical airfoils[C]//International Council of the Aeronautical Sciences Congress, 9th. Haifa, Israel: ICAS, 1974.[2] Dang T H. Development of NASA supercritical airfoils[J]. Design and Investigation of Civil Aircraft, 2005(2): 29-49 (in Chinese). 党铁红. NASA超临界翼型的发展[J]. 民用飞机设计与研究, 2005(2): 29-49.[3] Harris C D. NASA supercritical airfoils, NASA Technical Paper 2969[R]. Washington, D. C.: NASA, 1990.[4] Omar E, Ziertem T, Mahal A. Two-dimensional wing-tunnel tests of a NASA supercritical airfoil with various high-lift systems, NASA/CR-2214[R]. Hampton: NASA Langley Research Center, 1973.[5] Cosenza C J, Kummeth L J. Transonic aircraft technology/TACT/ program[C]//AIAA, Aerodynamic Testing Conference 8th. Reston: AIAA, 1974.[6] Lores M E, Smith P R, Hicks R M. Supercritical wing design using numerical optimization and comparisons with experiment[C]//AIAA, Aerospace Sciences Meeting 17th. Reston: AIAA, 1979.[7] Lowrey R. Evolution of transport wings from C-130, C-141, C-5 to C-XX[C]//AIAA, The Evolution of Aircraft Wing Design: Proceedings of the Symposium. Reston: AIAA, 1980.[8] Reaser J S, Hallissy J B, Campbell R L. Design and true Reynolds number 2-D testing of an advanced technology airfoil[C]//AIAA,Applied Aerodynamics Conference. Reston: AIAA, 1983.[9] Tranen T L. A rapid computer aided transonic airfoil design method[C]//AIAA, Fluid and Plasma Dynamic Conference 7th. Reston: AIAA, 1974.[10] Carlson L A. Transonic airfoil design using cartesian coordinates[J]. Journal of Aircraft, 1976, 13(5): 349-356.[11] Sobieczky H, Yu N J, Fung K Y, et al. New method for designing shock-free transonic configurations[J]. AIAA Journal, 1979, 17(7): 722-729.[12] Weed R A, Carlson L A. Combined direct/inverse three dimensional transonic wing design with visous and wing/body effects, AD-A 165[R]. Bethesda, Maryland: David W. Taylor Naval Ship Research and Development Center, 1984.[13] Takanashi S. Iterative three-dimensional transonic wing design using intergral equations[J]. Journal of Aircraft, 1985, 22(8): 655-660.[14] Hua J. Investigation of supercritical wing and airfoil design[D]. Xi'an: Northwestern Polytechnical University, 1989 (in Chinese). 华俊. 跨音速机翼和翼型的设计研究[D]. 西安: 西北工业大学, 1989.[15] Jameson A. Aerodynamic design via control theory[J]. Journal of Scientific Computing, 1988, 3(3): 233-260.[16] Quagliarella D, Cioppa A D. Genetic algorithms applied to the aerodynamic design of transonic airfoils[J]. Journal of Aircraft, 1995, 32(4): 889-891.[17] Holst T L, Pulliam T H. Aerodynamic shape optimization using a real number encoded genetic algorithm[C]//AIAA, Applied Aerodynamics Conference 19th. Reston: AIAA, 2001.[18] Shinkyu J, Mitsuhiro M, Kazuomi Y. Efficient optimization design method using kriging model[J]. Journal of Aircraft, 2005, 42(2): 413-420.[19] Wang X P, Gao Z H. Aerodynamic optimization design of airfoil based on genetic algorithm[J]. Acta Aerodynamica Sinica, 2000, 18(3): 324-329 (in Chinese). 王晓鹏, 高正红. 基于遗传算法的翼型气动优化设计[J]. 空气动力学学报, 2000, 18(3): 324-329.[20] Zhan H, Xu X P, Zhu J. Multi-point optimization for aerodynamic shape[J]. Aeronautical Computing Technique, 2007, 37(1): 19-21 (in Chinese). 詹浩, 许小平, 朱军. 气动外形多点优化设计研究[J]. 航空计算技术, 2007; 37(1): 19-21.[21] Bai J Q, Wang B, Sun Z W, et al. The research of robust supercritical airfoil design optimization[J]. Acta Aerodynamica Sinica, 2011, 29(4): 459-463 (in Chinese). 白俊强, 王波, 孙智伟, 等. 超临界翼型稳健型优化设计研究[J]. 空气动力学学报, 2011, 29(4): 459-463.[22] Huang Y, Chen Z B. An investigation for the complex-variable method in shape optimization of transonic airfoils[J]. Acta Aerodynamica Sinica, 2005, 23(4): 501-505 (in Chinese). 黄勇, 陈作斌. 跨声速翼型优化设计的复变量方法应用研究[J]. 空气动力学学报, 2005, 23(4): 501-505.[23] Qiao Z D. Design and choosen of the airfoils[M]//Fang B R. Aircraft Aerodynamic Configuration Design. Beijing: Aviation Industry Press, 1997: 499-540 (in Chinese). 乔志德. 翼型的选择与设计[M]//方宝瑞. 飞机气动布局设计. 北京: 航空工业出版社, 1997: 499-540.[24] Shen K Y, Zhang X H. Aerodynamic design criteria, design procedures and a design example of supercritical wing[J]. Acta Aeronautica et Astronautica Sinica, 1993, 14(4): 113-117 (in Chinese). 沈克杨, 张锡华. 超临界机翼气动设计的准则、流程和设计实例[J]. 航空学报, 1993, 14(4): 113-117.[25] Chen Y C, Si J T, Han X L, et al. Investigation of transition effect on the pressure distribution of supercritical wing[J]. Acta Aerodynamica Sinica, 2003, 21(4): 470-475 (in Chinese). 陈迎春, 司江涛, 韩先锂,等. 转捩对超临界机翼压力分布的影响分析[J]. 空气动力学学报, 2003, 21(4): 470-475.[26] Chen S, Bai J Q, Sun Z W, et al. Aerodynamic optimization design of airfoil using DFFD technique[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(3): 695-705 (in Chinese). 陈颂, 白俊强, 孙智伟, 等. 基于DFFD技术的翼型气动优化设计[J]. 航空学报, 2014, 35(3): 695-705.[27] Yang K M, Zhang W M, Wang B. Research of supercritical wing optimization based on aerodynamic design principle of wing[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(2): 263-272 (in Chinese). 杨昆淼, 张卫民, 王斌. 基于机翼气动设计准则的超临界机翼气动优化研究[J]. 航空学报, 2013, 34(2): 263-272.[28] Li J, Gao Z H, Huang J T, et al. Aerodynamic optimization system based on CST technique[J]. Acta Aerodynamica Sinica, 2012, 30(4): 443-449 (in Chinese). 李静, 高正红, 黄江涛, 等. 基于CST参数化方法气动优化设计研究[J]. 空气动力学学报, 2012, 30(4): 443-449.[29] Shi Q, Li H. Numerical simulation on action of flow control and wave drag reduction effect with contour bump located on the supercritical airfoil[J]. Acta Aerodynamica Sinica, 2010, 28(4): 462-465 (in Chinese). 石清, 李桦. 实体鼓包对超临界翼型的流动控制和减阻研究[J]. 空气动力学学报, 2010, 28(4): 462-465.[30] Gao Z H, Bai J Q. C919 airplane airfoil design and analysis report[R]. Xi'an: Northwestern Polytechnical University,National Key Laboratory of Aerodynamic Design and Research, 2008 (in Chinese). 高正红, 白俊强. C919大型客机翼型设计分析报告[R]. 西安: 西北工业大学,翼型叶栅空气动力国防科技重点实验室, 2008.[31] Burdges K P. A synthesis of transonic, 2-D airfoil technology[C]//AIAA Aircraft Design, Flight Test and Operations Meeting 5th. Reston: AIAA, 1973.[32] Obert E. Aerodynamic design of transport aircraft[M]. Netherlands: IOS Press, 2009: 75-106.[33] Zhang Y F. Aerodynamic optimization of civil aircraft design based on advanced computational fluid dynamics[D]. Beijing: Tsinghua University, 2010 (in Chinese). 张宇飞. 基于先进CFD方法的民用客机气动优化设计[D]. 北京: 清华大学, 2010.[34] Kulfan B M. A universal parameteric geometry representation method-"CST"[C]//AIAA Aerospace Sciences Meeting and Exhibit 45th. Reston: AIAA, 2007.[35] Kulfan B M, Bussoletti J E. "Fundamental" parametric geometry representations for aircraft component shapes[C]//AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 11th. Reston: AIAA, 2006.[36] Bai J Q, Yin G L, Sun Z W. Random weighted hybrid particle swarm optimization algorithm based on second order oscillation and natural selection[J]. Control and Decision, 2012, 27(10): 1459-1464 (in Chinese). 白俊强, 尹戈玲, 孙智伟. 基于二阶振荡及自然选择的随机权重混合粒子群算法[J]. 控制与决策, 2012, 27(10): 1459-1464.[37] Chao D D, Dam C P. Airfoil drag prediction and decomposition[J]. Journal of Aircraft, 1998, 36(4): 675-681.[38] Cook P H, McDonald M A, Firmin M C P. Aerofoil RAE 2822—pressure distributions, and boundary layer and wake measurements, AGARD AR-138[R]. Neuilly Sur Seine, France: AGARD, 1979.[39] Smith R E. Transfinite interpolation (TFI) generation systems[M]//Thompson J F, Soni B K, Weatherill N P. Handbook of Grid Generation. New York: CRC Press, 1998:108-122. |
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