BUCHER C G,BOURGUND U.Fast and efficient response surface approach for structural reliability problems[J].Struc- tural Safety,1990,7(1):57-66.
[2]
LIU B,HAFTKA R T.Single-level composite wing optimization based on flexural lamination parameters[J].Structural and Multidisciplinary Optimization,2004,26(1):111-120.
[3]
王海亮,林忠钦,金先龙.基于响应面模型的薄壁构件耐撞性优化设计[J].应用力学学报,2003,20(3):61-65.WANG Hai-liang,LIN Zhong-qin,JIN Xian-long.Optimal design of thin-walled sections for structural crashworthiness based on the response surface model[J].Chinese Journal of Applied Mechanics,2003,20(3):61-65.(in Chinese)
[4]
ROUX W J,NIELEN S,HAFTKA R T.Response surface approximations for structural optimization[J].International Journal for Numerical Methods in Engineering,1998,42(3):517-534.
[5]
MYERS R H,MONTGOMERY D C.Response surface methodology[M].New York:John Wiley,1995.
[6]
LIU Y W,MOSES F.Sequential response Surface method and its application in the reliability analysis of aircraft structural systems[J].Structural Safety,1994,16(1):39-46.
[7]
KAUFMAN M,BALABANOV V,BURGEE S L,et al.Variable-complexity response Surface approximations for wing structural weight in HSCT design[J].Computational Mechanics,1996,18(2):112-126.
[8]
LIU B,HAFTKA R T,AKGUN M A.Two-level composite wing structural optimization using response surfaces[J].Struc- tural and Multidisciplinary Optimization,2000,20(2):87-96.