| Citation: | MA Yang, WANG Dan-dan, YANG Tao, FENG Zhi-wei, ZHANG Qing-bin. Optimization design of shroud configuration of transporter based on surrogate model[J]. Journal of Aerospace Power, 2014, 29(1): 192-198. doi: 10.13224/j.cnki.jasp.2014.01.025
|
| [1] |
夏露, 高正红, 李天.飞行器外形多目标多学科综合优化设计方法研究[J].空气动力学学报, 2003, 21(3):275-281. XIA Lu, GAO Zhenghong, LI Tian.Research on multi-objective and multi-disciplinary optimization design of aircraft configuration[J].Acta Aerodynamica Sinica, 2003, 21(3):275-281.(in Chinese)
|
| [2] |
唐伟, 高晓成, 李为吉.双椭圆截面再入飞行器的气动计算及布局优化设计[J].空气动力学学报, 2004, 22(2):171-174. TANG Wei, GAO Xiaocheng, LI Weiji.Aerodynamics prediction and configuration optimization for reentry vehicle with double-ellipse cross-section[J].Acta Aerodynamica Sinica, 2004, 22(2):171-174.(in Chinese)
|
| [3] |
唐伟, 桂业伟, 方方.新型升力再入飞船返回舱气动外形选型研究[J].宇航学报, 2008, 29(1):84-88. TANG Wei, GUI Yewei, FANG Fang.Aerodynamic configurations selection for lift reentry capsule[J].Journal of Astronautics, 2008, 29(1):84-88.(in Chinese)
|
| [4] |
王允良, 张勇, 李为吉.可重复使用运载器机翼外形优化[J].宇航学报, 2004, 25(5):488-491. WANG Yunliang, ZHANG Yong, LI Weiji.Wing shape optimization of the reusable launch vehicle[J].Journal of Astronautics, 2004, 25(5):488-491.(in Chinese)
|
| [5] |
Theisinger J E, Braun R D.Multi-objective hypersonic entry aeroshell shape optimization[J].Journal of Spacecraft and Rockets, 2009, 46(5):957-966.
|
| [6] |
曾会华, 余雄庆.基于代理模型的气动外形优化[J].航空计算技术, 2005, 35(4):84-87. ZENG Huihua, YU Xiongqing.An approach to aerodynamic shape optimization using surrogate models[J].Aeronautical Computer Technique, 2005, 35(4):84-87.(in Chinese)
|
| [7] |
杨华.机翼气动力双向代理模型设计[D].南京:南京航空航天大学, 2007. YANG Hua.2D surrogate model design of aerodynamic force of air-foil[D].Nanjing:Nanjing University of Aeronautics and Astronautics, 2007.(in Chinese)
|
| [8] |
李晓宇, 欧海英, 丁国昊.基于响应面方法的高超声速飞行器一体化布局气动设计与优化[J].导弹与航天运载技术, 2010, 306(2):8-11. LI Xiaoyu, OU Haiying, DING Guohao.Integrative aerodynamic design and optimization of hypersonic vehicle configurations based on response surface methodology[J].Missile and Space Vehicles, 2010, 306(2):8-11.(in Chinese)
|
| [9] |
Wesseling P.Principles of computational fluid dynamics[M].Berlin:Springer-Verlag Berlin Heidelberg, 2001.
|
| [10] |
Azevedo J L F, Moraes P Jr.Code validation for high-speed flow simulation over satellite launch vehicle[J].Journal of Spacecraft and Rockets, 1996, 30(1):15-21.
|
| [11] |
穆雪峰.多学科设计优化代理模型技术的研究和应用[D].南京:南京航空航天大学, 2004. MU Xuefeng.Surrogate model study and application in multi-disciplinary design optimization[D].Nanjing:Nanjing University of Aeronautics and Astronautics, 2004.(in Chinese)
|
| [12] |
Tang B.Orthogonal array-based latin hypercubes[J].Journal of the American Statistical Association, 1993, 88(424):1392-1397.
|
| [13] |
杨劼, 戴全辉, 黄兴军.一种基于参数化建模的飞行器隐身外形设计优化方法[J].战术导弹技术, 2009(2):1-5. YANG Jie, DAI Quanhui, HUANG Xingjun.An approach to stealth shape design and optimization for flying vehicle based on parametric modeling[J].Tactical Missile Technology, 2009(2):1-5.(in Chinese)
|
| [14] |
Fares R, CHEN Xiaoming, Agarwal R.Shape optimization of an axisymmetric diffuser and a 3D hydro-turbine draft tube using a genetic algorithm[C]//49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.Orlando:AIAA, 2011:4-7.
|
| [15] |
Ahmed M Y M, Qin N.Surrogate-based multi-objective aerothermodynamic design optimization of hypersonic spiked bodies[R].AIAA Journal, 2012, 50(4):797-810.
|
| [16] |
Deb K, Pratap A, Agrawal S.A fast and elitist multi-objective genetic algorithm:NSGA-Ⅱ[J].Transactions on Evolutionary Computation, 2000, 6(2):182-197.
|
DownLoad: