[1] 樊会涛,王起飞.远程空空导弹的发展及其关键技术[J].航空兵器,2006(1):3-7.FAN H T,WANG Q F.Development and key technology of long-range air-to-air missile[J].Aero Weaponry,2006(1):3-7(in Chinese).
[2] 李国雄.吸气式远程超声速防空导弹一体化外形设计的几个重大技术问题[J].现代防御技术,2002,30(2):29-34.LI G X.Several important technical questions in integrated configuration design of air-breathing long-range supersonic surface-to-air missiles[J].Modern Defence Technology,2002,30(2):29-34(in Chinese).
[3] 王明鉴.整体式固冲发动机与导弹一体化优化设计[J].固体火箭技术,1997,20(2):7-13.WANG M J.The integrated design optimization of solid rocket ramjet and missile[J].Journal of Solid Rocket Technology,1997,20(2):7-13(in Chinese).
[4] 赵建民,夏智勋,郭健,等.基于全模式遗传算法的导弹/固体冲压发动机一体化优化[J].固体火箭技术,2005 28(1):1-4.ZHAO J M,XIA Z X,GUO J,et al.Integral design optimization for missile/solid rocket ramjet based on all schema genetic algorithm[J].Journal of Solid Rocket Technology,2005,28(1):1-4(in Chinese).
[5] 谷良贤,李文华.整体式固冲发动机空空导弹一体化设计[J].战术导弹技术,1997(4):1-4.GU L X,LI W H.Integral design of air-to-air missile with integrate rocket ramjet[J].Tactical Missile Technology,1997(4):1-4(in Chinese).
[6] BESSER H L.History of ducted rocket development at Bayern-Chemie:AIAA-2008-5261[R].Reston:AIAA,2008.
[7] SOBIESKI J,HAFTKA R T.Multidisciplinary aerospace design optimization:survey of recent developments:AIAA-1996-0711[R].Reston:AIAA,1996.
[8] THOMAS A Z,LAWRENCE L G.Multidisciplinary design optimization techniques:implications and opportunities for fluid dynamics research:AIAA-1999-3798[R].Reston:AIAA,1999.
[9] 熊俊涛,乔志德,韩忠华.基于响应面法的跨声速机翼气动优化设计[J].航空学报,2006,27(3):399-402.XIONG J T,QIAO Z D,HAN Z H.Optimum aerodynamic design of transonic wing based on response surface methodology[J].Acta Aeronautica et Astronautica Sinica,2006,27(3):399-402(in Chinese).
[10] 蒙文巩,马东立,楚亮.基于神经网络响应面的机翼气动稳健性优化设计[J].航空学报,2010,31(6):1134-1140.MENG W G,MA D L,CHU L.Wing aerodynamic robustness optimization based on neural network response surface[J].Acta Aeronautica et Astronautica Sinica,2010,31(6):1134-1140(in Chinese).
[11] MYERS R H,MONTGOMERY D C.Response surface methodology:process and product optimization using designed experiments[M].New York:John Wiley & Sons,1995:28-31,79-133.
[12] KIM H.Statistical modeling of simulation errors and their reduction via response surface techniques[D].Blacksburg,Virginia:Virginia Polytechnic Institute and State University,2001:22-32.
[13] GIUNTA A A.Aircraft multidisciplinary design optimization using design of experiments theory and response surface modeling methods[D].Blacksburg,Virginia:Virginia Polytechnic Institute and State University,1997:36-42.
[14] 鲍福廷,黄熙君,张振鹏,等.固体火箭冲压组合发动机[M].北京:中国宇航出版社,2006:292-312.BAO F T,HUANG X J,ZHANG Z P,et al.Integral solid propellant ramjet rocket motor[M].Beijing:China Astronautic Publishing House,2006:292-312(in Chinese). |