[1] Hicks R M, Murman E M, Vanderplaats G N. An assessment of airfoil design by numerical optimization. NASA-TM-X-3092, 1974.
[2] Hicks R M, Henne P. Wing design by numerical optimization[J]. Journal of Aircraft, 1978, 15(7): 407-412.
[3] Jameson A. Aerodynamic design via control theory[J]. Journal of Scientific Computing, 1988, 13(3): 233-260.
[4] 刘润泽, 张晓东, 安柏涛, 等. 非均匀有理B样条曲线及节点插入算法在透平叶片优化设计中的应用[J]. 航空动力学报, 2010, 25(2): 451-458. Liu Runze, Zhang Xiaodong, An Botao, et al. Application of non-uniform rational B-spline curve and knot insertion algorithm to turbine blade optimization[J]. Journal of Aerospace Power, 2010, 25(2): 451-458. (in Chinese)
[5] Samareh J A. A survey of shape parameterization techniques for high-fidelity multidisciplinary shape optimization[J]. AIAA Journal, 2001, 39(5): 877-884.
[6] Wataru Y, Sylvain M, Gérald C. Geometry parameterization and computational mesh deformation by physics-based direct manipulation approaches[J]. AIAA Journal, 2010, 48(8): 1817-1832.
[7] Jason E H, David W Z. Aerodynamic optimization algorithm with integrated geometry parameterization and mesh movement[J]. AIAA Journal, 2010, 48(2): 400-413.
[8] 王晓锋, 席光. 基于Kriging模型的翼型气动性能优化设计[J]. 航空学报, 2005, 26(5): 545-549. Wang Xiaofeng, Xi Guang. Aerodynamic optimization design for airfoil based on Kriging model[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(5): 545-549. (in Chinese)
[9] 杨旭东, 乔志德. 基于共轭方程法的跨音速机翼气动力优化设计[J]. 航空学报, 2003, 34(1): 2-5. Yang Xudong, Qiao Zhide. Optimum aerodynamic design of transonic wing based on adjoint equations method[J]. Acta Aeronautica et Astronautica Sinica, 2003, 34(1): 2-5. (in Chinese)
[10] 孙奕捷, 申功璋. 飞翼布局飞机控制/气动/隐身多学科优化设计[J]. 北京航空航天大学学报, 2009, 35(11): 1357-1360. Sun Yijie, Shen Gongzhang. Multidisciplinary optimization of control-aerodynamic-stealth for flying wing aircraft design[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(11): 1357-1360. (in Chinese)
[11] Vijay N J, Felipe A C V, Raphael T H, et al. Design optimization of a bendable UAV wing under uncertainty. AIAA-2010-2761, 2010.
[12] Kim H J, Liou M S. Aerodynamic optimization using a hybrid moga-local search method. AIAA-2010-2911, 2010.
[13] Laurenceau J, Meaux M, Montagnac M, et al. Comparison of gradient-based and gradient-enhanced response-surface-based optimizers[J]. AIAA Journal, 2010, 48(5): 981-994.
[14] Jameson A, Martinelli L, Pierce N A. Optimum aerodynamic design using the Navier-Stokes equations[J]. Theoretical and Computational Fluid Dynamics, 1998(10): 213-237.
[15] Leoviriyakit K, Jameson A. Multi-point wing planform optimization via control theory. AIAA-2005-450, 2005.
[16] Takenaka K, Obayashi S, Nakahashi K, et al. The application of MDO technologies to the design of a high performance small jet aircraft. AIAA-2005-4797, 2005.
[17] Jason E H, David W Z. Integrated geometry parametrization and grid movement using B-spline meshes. AIAA-2008-6079, 2008.
[18] Lepine J, Guibault F, Trepanier J, et al. Optimized non-uniform rational B-spline geometrical representation for aerodynamic design of wings[J]. AIAA Journal, 2001, 39(11): 2033-2041.
[19] Castonguay P, Nadarajah S. Effect of shape parameterization on aerodynamic shape optimization. AIAA-2007-59, 2007.
[20] Arash M, Patrice C, Siva K N. Survey of shape parameterization techniques and its effect on three-dimensional aerodynamic shape optimization. AIAA-2007-3837, 2007.
[21] Pandya M J, Baysal O. Gradient-based aerodynamic shape optimization using alternating direction implicit method[J]. Journal of Aircraft, 1997, 34(3): 346-352.
[22] Baldwin B S, Lomax H. Thin layer approximation and algebraic model for separated turbulent flows. AIAA-1978-257, 1978.
[23] Chakravarthy S R, Osher S. Numerical experiments with the Osher upwind scheme for the Euler equations[J]. AIAA Journal, 1983, 21(9): 1241-1248.
[24] Jameson A. Aerodynamic design via control theory[J]. Journal of Scientific Computing, 1988, 3(3): 233-260.
[25] Wilson R B. A simplicial algorithm for concave programming. Boston: Harvard University, 1963. |