[1] MOHAMMD A Z, BREZILLON J. Shape optimization usingthe aerostructural coupled adjoint approach for viscous flow[C] //Proceedings of Evolutionary and Deterministic for Design, Optimization and Con-trol, 2011.[2] LEOVIRIYAKIT K, JAMESON A. Case studies in aerostructural wing planform and section optimization. AIAA-200405372[R]. Reston, VA:AIAA 2004.[3] MELVIN R G, HUFFMAN WP. Recent progress in aerodynamic design optimization[J]. Int J Number Meth Fluids, 1999, 30(2):205-216. [4] 周铸,黄江涛,高正红等.民用飞机气动外形数值优化设计面临的挑战与展望[J]. 航空学报, 2019, 40(1):522370-522370. ZHOU Z, HUANG J T, GAO Z H, et al. Challenges and prospects of numerical optimization design for laorge civil aircraft aerodynamic shape[J]. Acta Aero-nautica et Astronautica Sinica, 2019, 40(1):522370-522370 (in chinese). Doi:10.7527/s1000-6839. 2018. 22370.[5] STEPHEN T, LEDOUX, WILLIAM W. et al. MDOPT-a multidisciplinary design optimization system using higher order analysis codes[C]. AIAA Paper 98-4757, August 2004, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.[6] GRAY J, MOOREY K T, NAYLOR B A. OpenMDAO: An open source framework for multidisciplinary analysis and Optimization[C]. Proceedings of 13th AIAA/ISSMO Multidisciplinary Analysis Optimiza-tion Conference. 2010, Fort Worth, Texas, USA: AIAA.[7] JAMESON J, PIERCE N A., MARTINELLI L. Opti-mum aerodynamics design using the Navier-Stokes equations: AIAA-97-0101[R]. Reston, VA:AIAA, 1997.[8] NIELSEN E J, ANDERSON W K. Recent improve-ments in aerodynamic design optimization on un-structured meshes: AIAA-2001-0596, 2000[R]. Reston, VA:AIAA.[9] 黄江涛, 周铸, 刘刚, 等.飞行器气动/结构多学科延迟耦合伴随系统数值研究[J]. 航空学报, 2018, 39(5):121731-121731..HUANG J T, ZHOU Z, LIU G, et al. Numerical study of aero-structural multidisciplinary lagged coupled adjoint system for aircraft[J]. Acta Aeronautica et As-tronautica Sinica, 2018, 39(5):121731-121731 (in chinese). Doi:10.7527/S1000-6893.2017.21731.[10] COELLO COELLO CA, VAN VELDUIZEN DA, LAMONT GB. Evolutionary algorithms for solving multi-Objective problems[M]. Kluwer Academic Pub-lishers, New York, May 2002.[11] 郑传宇, 黄江涛, 周铸, 等. 飞翼翼型高维多目标空间多学科综合优化设计[J]. 空气动力学学报, 2017, 35(4):587-597. Doi:10.7638/kqdlxxb-2017.0079. ZHENG C Y, HUANG J T, ZHOU Z, et al. Multidisci-plinary optimization design of high dimensional target space for flying wing airfoil[J]. Acta Aerodynamica Sinica, 2017, 35(4):587-597. [12] Sobieszczanski-Sobieski J. Sensitivity analysis and multidisciplinary optimization for aircraft design: re-cent advance and results[J]. Journal of Aircraft, 1990,27(12):993-1001.[13] LES PIEGL, WAYNE TILLER. The NURBS Book[M], Springer, 1997.[14] BRENDA MKULFAN. Recent extensions and appli-cations of the “CST” universal parametric geometry representation method[C]: AIAA-2007-7709[R]. Reston, VA:AIAA, 2007.[15] SEDERBERG T W, PARRY S R. Freeform deforming of solid geometric models[J]. Computer Graphics, 1986, 22(4):151-160.[16] J A SAMAREH. Aerodynamic shape optimization based on Free-Form Deformation[C]: AIAA-2004-4630,[R]. Reston, VA:AIAA, 2004.[17] PANG Y F, ZHANG S J, SUN J F. An adaptive grid rebuilding method for multi-zone structured grid[C]. 6th Asia Workshop on Computational Fluid Dynamics, 2006.[18] 肖涵山, 陈作斌, 刘刚, 江雄. 基于Euler方程的三维自适应笛卡尔网格应用研究[J]. 空气动力学学报, 2003, 21(2):202-210. XIAO H S, CHEN Z B, LIU G, et al. Applications of 3-D adaptive Cartesian grid algorithm based on the Euler equations[J]. Acta Aerodynamica Sinica, 2003, 21(3):202-210. [19] 牟斌, 肖中云, 周铸, 等. 多重网格技术在复杂粘性流场计算中的应用及研究[J]. 空气动力学学报, 2006, 24(1):51-54. MOU B, XIAO Z Y, ,ZHOU Z, et al. Application and investigation of multi-block multi-grid method in complicated viscous flow fields calculation[J]. Acta Aerodynamica Sinica, 2006, 24(1):51-54 . [20] M D MCKAY, W J CONOVER, R J BECKMAN. A comparison of three methods for selecting values of input variables in the analysis of output from a com-puter code[J]. Technometrics, 1979, 21(3): 239–245.[21] 方开泰,马长兴. 正交与均匀试验设计[M]. 北京: 科学与试验出版社,1980. FANG K T, MA C X. Orthogonal and uniform exper-imental design[M]. Beijing: Science Press, 1980 (in Chinese). [22] SHINKYU JEONG, MITSUHIRO MURAYMA. Efficient optimization design method using Kriging model. Journal of Aircraft , 2005,42(2):413-420.[23] 黄江涛, 高正红, 余婧, 等. 大型民用飞机气动外形典型综合设计方法[J]. 航空学报, 2019, 40(2):522369-522369. HUANG J T, GAO Z H , YU J, et al. A typical inte-grated design method design method for aerodynam-ics shape optimization of large civil aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(2):522369-522369 ( in chinese). [24] 黄江涛, 周铸, 余婧, 等. 考虑飞行器动力系统进排气效应的设计参数灵敏度分析研究[J]. 推进技术, 2019, 40(2):250-258. HUANG J T, ZHOU Z, YU J, et al. Sensitivity analy-sis of design variables considering intake and exhaust effects[J]. Journal of propulsion technology, 2019,40(2): 250-258 (in chinese). |