| Citation: | TAN Xiang-fei, HE Yu-ting, FENG Yu, ZHANG Hao-yu, AN Tao. Buckling and post-buckling performance of aeronautic carbon fiber reinforced resin composite stiffened panel under compression[J]. Journal of Aerospace Power, 2016, 31(10): 2359-2369. doi: 10.13224/j.cnki.jasp.2016.10.008 |
| [1] |
王菲菲,崔得刚,熊强,等.复合材料加筋板后屈曲承载能力工程分析方法[J].北京航空航天大学学报,2013,39(4):494-497. WANG Feifei,CUI Degang,XIONG Qiang,et al.Engineering analysis of post-buckling loading capability for composite stiffened panels[J].Journal of Beijing University of Aeronautics and Astronautics,2013,39(4):494-497.(in Chinese)
|
| [2] |
霍世慧,王富生,王佩艳,等.复合材料机翼加筋壁板稳定性分析[J].应用力学学报,2010,27(2):423-427. HUO Shihui,WANG Fusheng,WANG Peiyan,et al.Stability analysis on the ribbed panel of the composite wing[J].Chinese Journal of Applied Mechanics,2010,27(2):423-427.(in Chinese)
|
| [3] |
冯宇,何宇廷,邵青,等.航空复合材料加筋板压缩屈曲及后屈曲性能[J].航空动力学报,2014,29(12):2905-2913. FENG Yu,HE Yuting,SHAO Qing,et al.Buckling and post-buckling performance of aeronautic composite stiffened panel under compression[J].Journal of Aerospace Power,2014,29(12):2905-2913.(in Chinese)
|
| [4] |
孔斌,陈普会,陈炎.复合材料整体加筋板轴压后屈曲失效评估方法[J].复合材料学报,2014,31(3):765-771. KONG Bin,CHEN Puhui,CHEN Yan.Post-buckling failure evaluation method of integrated composite stiffened panels under uniaxial compression[J].Acta Materiae Compositae Sinica,2014,31(3):765-771.(in Chinese)
|
| [5] |
朱菊芬,杨海平.复合材料层合加筋板结构的后屈曲强度及破坏研究[J].航空学报,1995,16(1):118-122. ZHU Jufen,YANG Haiping.A study of post-buckling strength and failure for composite stiffened plates structures[J].Acta Aeronautica et Astronautica Sinica,1995,16(1):118-122.(in Chinese)
|
| [6] |
沈惠申.复合材料层合厚板后屈曲[J].上海交通大学学报,1998,32(11):78-83. SHEN Huishen.Post-buckling of composite laminated thick plates[J].Journal of Shanghai Jiao Tong University,1998,32(11):78-83.(in Chinese)
|
| [7] |
冯宇,何宇廷,安涛,等.湿热环境对航空复合材料加筋板压缩屈曲和后屈曲性能的影响[J].材料工程,2015,43(5):81-88. FENG Yu,HE Yuting,AN Tao,et al.Influence of hygrothermal environment on compressive buckling and post-buckling performance of aero composite stiffened panel[J].Journal of Materials Engineering,2015,43(5):81-88.(in Chinese)
|
| [8] |
刘璐,关志东,徐荣章,等.脱胶缺陷尺寸对复合材料加筋板屈曲及后屈曲特性的影响[J].复合材料学报,2014,31(3):749-758. LIU Lu,GUAN Zhidong,XU Rongzhang,et al.Effect of debond size on buckling and post-buckling behaviors of composite stiffened panels[J].Acta Material Compositae Sinica,2014,31(3):749-758.(in Chinese)
|
| [9] |
Lanzi L.A numerical and experimental investigation on composite stiffened panels into post-buckling[J].Thin-Walled Structures,2004,42(12):1645-1664.
|
| [10] |
Orifici A C,De Zarate A O,Thomson R S,et al.Compression and post-buckling damage growth and collapse analysis of flat composite stiffened panels[J].Composites Science and Technology,2008,68(15/16):3150-3160.
|
| [11] |
Orifici A C,Thomson R S,Herszberg I,et al.An analsis methodology for failure in post-buckling skin stiffener interfaces[J].Composite Structures,2008,86(1):186-193.
|
| [12] |
Orifici A C,Thomson R S,Degenhardt R,et al.Degradation investigation in a postbuckling composite stiffened fuselage panel[J].Composite Structures,2008,86(2):217-224.
|
| [13] |
沈观林,胡更开,刘彬.复合材料力学[M].北京:清华大学出版社,2006.
|
| [14] |
克里斯托斯·卡萨波格罗.飞机复合材料结构设计与分析[M].颜万亿,译.上海:上海交通大学出版社,2011.
|
| [15] |
Megson T H G.Aircraft structures for engineering students[M].3rd ed.Amsterdam:Elsevier Ltd.,2007.
|
| [16] |
Whitney J M.Structural analysis of laminated anisotropic plates[M].Lancaster,PA:Technomic Publishing Company,1987.
|
| [17] |
Herakovich C T.Mechanics of fibrous composites[M].5th ed.New York:John Wiley and Sons Inc.,1998.
|
| [18] |
Timoshenko P S, Gere J M.Theory of elastic stabiity[M].New York:Dover Publications Inc.,2009.
|