Bi-point/bi-objective optimization design of ailfoil using N-S equations

[1] 刘周,朱自强,付鸿雁,等.高升阻比翼型的设计[J].空气动力学学报,2004,22(4):410-415 Liu Zhou,Zhu Ziqiang,Fu Hongyan,et al.Design of airfoil with high ratio of lift over drag[J].Acta Aerodynamica Sinica,2004,22(4):410-415(in Chinese) [2] Tinoco E N. An assessment of CFD prediction of drag and other longitudinal characteristics . AIAA 2001-1002,2001 [3] Sobieski J S. Optimization for engineering systems,achievements and potential . NASA TM 101566,1989 [4] Li P, OM D. Design application in the industry IUTAM Symposium Transsonicum Ⅳ. Dordrecht:Kluwer Academic Publishers, 2003:231-238 [5] Van Dam C P. Recent experience with different methods of drag prediction[J]. Progress in Aerospace Sciences, 1999, 35:751-798 [6] Van Dam C P, Nikfetrat K, Wong K, et al. Drag prediction at subsonic and transonic speeds using Euler methods[J]. Journal of Aircraft, 1995,32(4):839-845 [7] 刘杰,朱自强,陈泽民,等.基于欧拉方程的尾迹面法气动力计算[J].航空学报,2005,26(4):417-421 Liu Jie,Zhu Ziqiang,Chen Zemin, et al.Wake integration method for aerodynamics evaluation using Euler equations[J].Acta Aeronautica et Astronautica Sinica,2005,26(4):417-421(in Chinese) [8] Chao D D, Van Dam C P. Airfoil drag prediction and decomposition . AIAA 98-2783,1998 [9] 刘周,朱自强,王晓璐,等.基于N-S方程的尾迹面法翼型气动阻力计算 .北京航空航天大学 报,2006,26(3):288-292 Liu Zhou,Zhu ZIqiang,Wang Xiaolu,et al.Wake integration method for airfoil drag evaluation using N-S equations[J].Journal of Beijing University of Aeronautics and Astronautics,2006,26(3):288-292(in Chinese) [10] Jameson A, Schmidt W, Turkel E. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes . AIAA 81-1259,1981 [11] Baldwin B S, Lomax H. Thin layer approximation and algebraic model for separated turbulent flows . AIAA 78-257,1978 [12] Powell M J D. An efficient method for finding the minimum of a function of several variables without calculation derivatives[J]. Computer Journal, 1964, 7:155-162 [13] Zhu Z Q, Fu H Y, Yu R X, et al. Multi-objective optimization design of airfoil and wing[J]. Science in China(series E), 2004,47(1):15-25 [14] Zhu Z Q, Liu Z, Li H M, et al. Construction of integral objective function/fitness function of multi-objective/multi-disciplinary optimization . Computer Modeling in Engineering & Sciences, 2004,6(6):567-576 [15] Sobieczky H. Parametric airfoils and wings[J]. Note on Numerical Fluid Mechanics,1998,68:71-88