[1] Mousavi A, Castonguay P, Nadarajah S K. Survey of shape parameterization techniques and its effect on three-dimensional aerodynamic shape optimization. AIAA-2007-3837, 2007. [2] Samareh J A. Survey of shape parameterization techniques for high-fidelity multidisciplinary shape optimization. AIAA Journal, 2001, 39(5): 877-884. [3] Sripavadkul V, Padulo M, Guennov M. A comparison of airfoil shape parameterization techniques for early design optimization. AIAA-2010-9050, 2010. [4] Kulfan B M, Bussoletti J E. "Fundamental" parametric geometry representations for aircraft component shapes.AIAA-2006-6948, 2006. [5] Kulfan B M. Recent extensions and applications of the "CST" universal parametric geometry representation method. AIAA-2007-7709, 2007. [6] Kulfan B M. A universal parametric geometry representation method-"CST". AIAA-2007-62, 2007. [7] Lane A K, Marshall D D. A surface parameterization method for airfoil optimization and high lift 2D geometries utilizing the CST methodology. AIAA-2009-1461, 2009. [8] Ceze M, Hayashi M, Volpe E. A study of the CST parameterization characteristics. AIAA-2009-3767, 2009. [9] Straathof M H, van Tooren M J L, Voskuijl M, et al. Aerodynamic shape parameterisation and optimisation of novel configurations. Proceedings of the RAeS Aerodynamic Shape Parameterisation and Optimisation of Novel Configurations Conference. London: Royal Aeronautical Soc., 2008: 1-14. [10] Straathof M H, van Tooren M J L, Voskuijl M, et al. Development and implementation of a novel parametrization technique for multidisciplinary design initialization. AIAA-2010-3004, 2010. [11] Straathof M H, van Tooren M J L. Extension to the class-shape-transformation method based on B-splines. AIAA Journal, 2011, 49(4): 780-790. [12] Demengel G, Pouget J P. Mathematiques des courbes et des surfaces. Wang X D, translated. Beijing: Commercial Press, 2000: 109-112(in Chinese) Demengel G, Pouget J P. 曲线与曲面数学. 王向东, 译. 北京: 商务印书馆, 2000: 109-112. [13] Li Y, Zhang K F, Yu J F. Technology and applications of computer aided geometric design. Xi’an: Northwestern Polytechnical University Press, 2007: 30-32. (in Chinese) 李原, 张开富, 余剑锋. 计算机辅助几何设计技术及应用. 西安:西北工业大学出版社,2007: 30-32. [14] Piegl L, Tiller W. The NURBS book. Heidelberg: Springer, 1997: 411-413. [15] Hicks R, Henne P. Wing design by numerical optimization. Journal of Aircraft, 1978, 15(7): 407-412. [16] Sobieczky H, Parametric airfoils and wings. Notes on Numerical Fluid Mechanics, 1998, 68: 71-88. [17] Jones R T. Theory of wing-body drag at supersonic speeds. NACA-RM-A53H18A, 1953. [18] Chin W C. Supersonic wave-drag of planar singularity distributions. AIAA Journal, 1978,16(5): 482-487. [19] Nikolic V, Jumper E J. Zero-lift wave drag calculation using supersonic area rule and its modifications. AIAA-2004-217, 2004. [20] Kulfan B M. New supersonic wing far-field composite-element wave-drag optimization method, "FCE". AIAA-2008-132, 2008. |