[1] Leishman J G. Principles of helicopter aerodynamics. 2nd Edition. New York: Cambridge University Press, 2006:348-350. [2] Dadone L U. Design and analytical study of a rotor airfoil. NASA CR-2988, 1978. [3] Yamauchi G K, Johnson W. Trends of Reynolds number effects on two-dimensional airfoil characteristics for helicopter rotor analyses. NASA TM-84363, 1983. [4] Qian R Z, Qiao Z D, Chen Y C, et al. Rotor airfoil optimization design using Navier-Stokes equations. Flight Dynamics, 2004, 22(1): 26-29. (in Chinese) 钱瑞战, 乔志德, 陈迎春, 等. 基于N-S方程的旋翼翼型优化设计方法. 飞行力学, 2004, 22(1): 26-29. [5] Huang H S, Yang X D. Optimum shape design of rotor airfoils via control theory. Aeronautical Computing Technique, 2010, 40(4): 22-26.(in Chinese) 黄海生, 杨旭东. 基于控制理论的旋翼翼型优化设计. 航空计算技术,2010,40(4): 22-26. [6] Hassan A A, Charles B D. Airfoil design for helicopter rotor blades-a three-dimensional approach. Journal of Aircraft, 1997, 34(2): 197-205. [7] Ranjan G L, Chopra I. Multi-objective optimization of a composite helicoper rotor. AIAA-1994-1420,1994. [8] Han Z H. Efficient method for simulation of viscous flows past helicopter rotors and active flow control. Xi’an: School of Aeronautics, Northwestern Polytechnical University, 2007. (in Chinese) 韩忠华. 旋翼绕流的高效数值计算方法及主动流动控制研究.西安:西北工业大学航空学院, 2007. [9] Spalart P R, Allmaras S R. A one equation turbulence model for aerodynamic flows. AIAA-1992-39, 1992. [10] Hicks R M, Henne P A. Wing design by numerical optimization. Journal of Aircraft, 1978, 15(7): 407-413. [11] Sobieczky H. Parametric airfoils and wings, recent development of aerodynamic design methodologies inverse design and optimization. Braunschweig Wiesbaden, Germany, Friedr: Vieweg & Sohn Verlagsgesellschaft mbH, 1999:72-74. [12] Lepine J, Guibault F, Trepanier, et al. Optimized nonuniform rational B-spline geometrical representation for aero-dynamic design of wings. AIAA Journal, 2001:39(11):2033-2041. [13] Giunta A A, Wojtkiewicz S F, Eldred M S, et al. Overview of modern design of experiments methods for computational simulations. AIAA-2003-649, 2003. [14] Jeong S, Murayama M, Yamamoto K. Efficient optimization design method using Kriging model. AIAA-2004-118, 2004. [15] Sekishiro M, Venter G, Balabanov V. Combined Kriging and gradient-based optimization method. AIAA-2006-7091, 2006. [16] Xu R F, Song W P, Han Z H. Application of improved Kriging-model-based optimization method in airfoil aerodynamic design. Journal of Northwestern Polytechnical University, 2010,28(4): 503-510. (in Chinese) 许瑞飞, 宋文萍, 韩忠华. 改进Kriging模型在翼型气动优化设计中的应用研究. 西北工业大学学报, 2010,28(4): 503-510. [17] Pape A L, Pailhas G, David F, et al. Extensive wind tunnel measurements of dynamic stall phenomenon for the OA209 airfoil including 3D effects. 33rd European Rotorcraft Forum-ERF 2007 KAZAN, RUSSIE 11-13, 2007. |