[1] Harris C D. NASA supercritical airfoils a matrix of family-related airfoils. NASA TP 2969. Hampton, Virginia, USA: Langley Research Center, 1990. [2] Wang B. Optimization design of aerodynamic distribution for civil aircraft supercritical wing. Beijing: China Academy of Aerospace Aerodynamics, 2010.(in Chinese) 王斌. 大型客机超临界机翼气动力布局优化设计.北京: 中国航天空气动力技术研究院,2010. [3] Shen K Y, Zhang X H. Aerodynamic design criteria, design procedures and a design example of supercritical wing. Acta Aeronautica et Astronautica Sinica, 1993, 14(4):113-117.(in Chinese) 沈克扬,张锡华. 超临界机翼气动设计的准则、流程和设计实例. 航空学报, 1993, 14(4): 113-117. [4] Hicks R M, Murman E M, Vanderplaats G N. An assessment of airfoil design by numerical optimization. NASA TM X-3092, Moffette Field. California, USA: Ames Research Center, 1974. [5] Hicks R M, Henne P A. Wing design by numerical optimization. Seattle, Washington, USA: AIAA Aircraft System & Technology Meeting, 1977. [6] Nieuwland G Y. Transonic potential flow around a family of quasi-elliptical aerofoil sections. NLR Technical Report T.172. Netherlands: NLR, 1967. [7] Tranen T L. A rapid computer-aided transonic airfoil design method. AIAA-1974-501, 1974. [8] Henne P A. Inverse transonic wing design method. Journal of Aircraft, 1981, 18(2): 121-127. [9] Zhu Z Q, Xia Z X, Wu L Y. An inverse design method of transonic airfoil and wing. Acta Aeronautica et Astronautica Sinica, 1992, 13(10): B463-B468.(in Chinese) 朱自强, 夏志勋, 吴礼义. 跨音速翼型和机翼的反设计计算方法.航空学报,1992,13(10): B463-B468. [10] Jameson A. Optimum aerodynamic design using CFD and control theory. AIAA-1995-1729, 1995. [11] Jameson A, Reuther J J, Martinelli L, et al. Aerodynamic shape optimization techniques based on control theory. AIAA-1998-2538, 1998. [12] Jameson A, Martinelli L, Cliff S, et al. Aerodynamic shape optimization of transonic and supersonic aircraft configurations. AIAA-2005-1013, 2005. [13] Yang X D, Qiao Z D, Zhu B. Aerodynamic design method based on control theory and Navier-Stokes equations. Acta Aerodynamica Sinica, 2005, 23(1): 46-51.(in Chinese) 杨旭东, 乔志德, 朱兵. 基于控制理论和NS方程的气动设计方法研究. 空气动力学报, 2005, 23(1): 46-51. [14] Cheng B S. 《Aircraft design manual》5th, civil aircraft design. Beijing: Aviation Industry Press, 2005: 110-112, 183-190.(in Chinese) 程不时.《飞机设计手册》第5册, 民用飞机总体设计. 北京: 航空工业出版社, 2005: 110-112, 183-190. [15] Zhang X J. 《Aircraft design manual》 6th, aerodynamic design. Beijing: Aviation Industry Press, 2005: 10-16, 30-32.(in Chinese) 张锡金.《飞机设计手册》第6册, 气动设计. 北京: 航空工业出版社, 2005: 10-16, 30-32. |