[1] |
沈观林,胡更开.复合材料力学[M].北京:清华大学出版社,2006.
|
[2] |
Sneha R P,Scott W C.Durability of a graphite/epoxy woven composite under combined hygrothermal conditions[J].International Journal of Fatigue,2000,22(9):809-820.
|
[3] |
Christian M.Closed-form buckling analysis of stiffened composite plates and identification of minimum stiffener requirements[J].International Journal of Engineering Science,2008,46(10):1011-1034.
|
[4] |
朱梅庄.复合材料结构设计手册[M].北京:航空工业出版社,2006.
|
[5] |
中国航空研究院.复合材料结构设计手册[M].北京:航空工业出版社,2001.
|
[6] |
Kong C W,Lee I C,Chun G,et al.Post-buckling and failure of stiffened composite panels under axial compression[J].Composite Structures,1998,42(1):13-21.
|
[7] |
Knight N F,Starnes J H.Postbuckling behavior of selected curved stiffened graphite-epoxy panels loaded in compression[J].AIAA Journal,1988,26(3):344-352.
|
[8] |
Adrian C O,Iligo O Z A,Rodney S T,et al.Compression and post-buckling damage growth and collapse analysis of flat composite stiffened panels[J].Composites Science and Technology,2008,68(15):3150-3160.
|
[9] |
石冶金,白瑞祥,王晓平,等.J型加筋壁板结构轴压试验及承载能力数值预测[J].工程力学,2013,30(2):413-418. SHI Yejin,BAI Ruixiang,WANG Xiaoping,et al.Experiment and load-carrying capability prediction for J shape stiffened composite plate under compression[J].Engineering Mechanics,2013,30(2):413-418.(in Chinese)
|
[10] |
张勇波,傅惠民,王治华.CCF300/QY8911单向纤维增强复合材料纵向压缩性能预测[J].航空动力学报,2013,28(6):1231-1235. ZHANG Yongbo,FU Huimin,WANG Zhihua.Compressive strength prediction of CCF300/QY8911 unidirectional fiber reinforced composite[J].Journal of Aerospace Power,2013,28(6):1231-1235.(in Chinese)
|
[11] |
傅惠民,杨雨松,张勇波.国产碳纤维CCF300与T300碳纤维复合材料拉伸载荷下的失效模式分析[J].航空动力学报,2010,25(10):2163-2169. FU Huimin,YANG Yusong,ZHANG Yongbo.Failure mode research on CCF300 and T300 composites under tensile strength[J].Journal of Aerospace Power,2010,25(10):2163-2169.(in Chinese)
|
[12] |
傅惠民,杨雨松,张勇波.含分层损伤国产碳纤维CCF300与T300碳纤维复合材料层合板压缩失效模式[J].航空动力学报,2011,26(11):2416-2421. FU Huimin,YANG Yusong,ZHANG Yongbo.Failure mode research on CCF300 and T300 carbon fiber composite laminates with delamination under compressive strength[J].Journal of Aerospace Power,2011,26(11):2416-2421.(in Chinese)
|
[13] |
孔斌,叶强,陈普会,等.复合材料整体加筋板轴压后屈曲的传载机制[J].复合材料学报,2010,27(5):142-149. KONG Bin,YE Qiang,CHEN Puhui,et al.Post-buckling load transfer mechanisms of an integrated composite panel under uniaxial compression[J].Acta Materiae Compositae Sinica,2010,27(5):142-149.(in Chinese)
|
[14] |
齐红宇,温卫东,齐红元,等.航空发动机复合材料机匣屈曲特性的有限元分析[J].航空动力学报,2001,16(4):335-339. QI Hongyu,WEN Weidong,QI Hongyuan,et al.FEM method for the critical buckling load of aeronautics composite case[J].Journal of Aerospace Power,2001,16(4):335-339.(in Chinese)
|
[15] |
郑亚雄,陈静,赵小全.复合材料薄壁加筋板的压缩后屈曲研究[J].直升机技术,2013,13(3):26-30. ZHENG Yaxiong,CHEN Jing,ZHAO Xiaoquan.Postbuckling analysis of thin-walled composite stiffened panels under compression[J].Helicopter Technique,2013,13(3):26-30.(in Chinese)
|
[16] |
Bisagni C,Lanzi C.Post-buckling optimisation of composite stiffened panels using neural networks[J].Composite Structures,2002,58(8):237-247.
|
[17] |
王春寿,陈普会,隋晓东,等.复合材料多墙盒段的设计与后屈曲性能[J].复合材料学报,2013,30(5):174-179. WANG Chunshou,CHEN Puhui,SUI Xiaodong,et al.Multi-spar composite box design and its post-buckling analysis[J].Acta Materiae Compositae Sinica,2013,30(5):174-179.(in Chinese)
|
[18] |
林淡.含冲击损伤层合板的剩余强度与疲劳研究[D].西安:西北工业大学,2013. LIN Dan.Study on the residual strength and fatigue of laminates with impact-damage[D].Xi'an:Northwestern Polytechnical University,2013.(in Chinese)
|