| Citation: | SHI Xiao-juan, JI Hong-hu. Optimization design of two dimensional convergent and divergent nozzles' profile based on surrogate models[J]. Journal of Aerospace Power, 2016, 31(9): 2124-2131. doi: 10.13224/j.cnki.jasp.2016.09.010
|
| [1] |
Hiley P E,Wallace H W,Booz D E.Study of non-axisymmetric nozzles installed in advanced fighter aircraft[R].AIAA 75-1316,1975.
|
| [2] |
Stevens H L,Thayer E B,Fullerton J F.Development of the multi-function 2-D/C-D nozzle[R].AIAA 81-1491,1981.
|
| [3] |
Capone F J.The nonaxisymmetric nozzle:it is for real[R].AIAA 79-1810,1979.
|
| [4] |
斯仁,吉洪湖,刘常春,等.冷却抑制二元收扩喷管红外特征的模型实验与数值研究[J].推进技术,2014,35(4):463-469. SI Ren,JI Honghu,LIU Changchun,et al.Model experiment and numerical analysis on infrared character and infrared suppression by cooling of two-dimensional convergent-divergent nozzle[J].Journal of Propulsion Technology,2014,35(4):463-469.(in Chinese)
|
| [5] |
《航空发动机设计手册》总编委会.航空发动机设计手册:第7册进排气装置[M].北京:航空工业出版社,2000.
|
| [6] |
吴达,郑克扬.排气系统的气动热力学[M].北京:北京航空航天大学出版社,1989.
|
| [7] |
施小娟,吉洪湖,斯仁.二元收扩喷管设计参数对气动性能影响的数值研究[J].航空动力学报,2016,31(8):1799-1810. SHI Xiaojuan,JI Honghu,SI Ren.Numerical investigation of geometric parameters' influence to aerodynamic performance of two dimensional convergent and divergent nozzles[J].Journal of Aerospace Power,2016,31(8):1799-1810.(in Chinese)
|
| [8] |
Simpson T W,Mauery T M,Korte J J,et al.Comparison of response surface and Kriging models for multidisciplinary design optimization[R].AIAA 98-4755,1998.
|
| [9] |
Simpson T W,Booker A J,Ghosh D,et al.Approximation methods in multidisciplinary analysis and optimization:a panel discussion[J].Structural and Multidisciplinary Optimization,2004,27(5):302-313.
|
| [10] |
余雄庆,丁运亮.多学科设计优化算法及其在飞行器设计中应用[J].航空学报,2000,21(1):1-6. YU Xiongqing,DING Yunliang.Multidisciplinary design optimization a survey of its algorithms and applications to aircraft design[J].Acta Aeronautica et Astronautica Sinica,2000,21(1):1-6.(in Chinese)
|
| [11] |
任超奇,王强,胡海洋.收-扩喷管与飞行器后体的一体化气动优化设计[J].航空动力学报,2014,29(10):2294-2302. REN Chaoqi,WANG Qiang,HU Haiyang.Integrated aerodynamic optimization design of convergent-divergent nozzle and vehicle afterbody[J].Journal of Aerospace Power,2014,29(10):2294-2302.(in Chinese)
|
| [12] |
穆雪峰,姚卫星,余雄庆,等.多学科设计优化中常用代理模型的研究[J].计算力学学报,2005,22(5):608-612. MU Xuefeng,YAO Weixing,YU Xiongqing,et al.A survey of surrogate models used in MDO[J].Chinese Journal of Computational Mechanics,2005,22(5):608-612.(in Chinese)
|
| [13] |
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 a aerodynamic shape optimization using surrogate models[J].Aeronautical Computer Technique,2005,35(4):84-87.(in Chinese)
|
| [14] |
杨俊杰,王荣桥,樊江,等.涡轮叶片的气动-热-结构多学科设计优化研究[J].航空动力学报,2010,25(3):617-622. YANG Junjie,WANG Rongqiao,FAN Jiang,et al.Multi-disciplinary aero-dynamic-thermal-structure design optimization for turbine blade[J].Journal of Aerospace Power,2010,25(3):617-622.(in Chinese)
|
| [15] |
韩永志,高行山,李立州,等.基于Kriging模型的涡轮叶片多学科设计优化[J].航空动力学报,2007,22(7):1055-1059. HAN Yongzhi,GAO Hangshan,LI Lizhou,et al.Kriging model-based multidisciplinary design optimization turbine blade[J].Journal of Aerospace Power,2007,22(7):1055-1059.(in Chinese)
|
| [16] |
黄章俊,王成恩.基于Kriging模型的涡轮盘优化设计方法[J].计算机集成制造系统,2010,16(5):905-911. HUANG Zhangjun,WANG Chengen.Turbine optimization design based on Kriging model[J].Computer Integrated Manufacturing Systems,2010,16(5):905-911.(in Chinese)
|
| [17] |
刘克龙,姚卫星,穆雪峰.基于Kriging代理模型的结构形状优化方法研究[J].计算力学学报,2006,23(3):344-347. LIU Kelong,YAO Weixing,MU Xuefeng.A method of structural shape optimization based on Kriging model[J].Chinese Journal of Computational Mechanics,2006,23(3):344-347.(in Chinese)
|
| [18] |
赖宇阳,姜欣,方立桥,等.Isight参数优化理论与实例详解[M].北京:北京航空航天大学出版社,2012.
|
DownLoad: