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	题名	作者	年代	出处	被引量
1	Developments in Composite Con-struction and Cellular Beams 显示文摘	LAWSON R M	2005	Steel and CompositeStructures2005，5，23：	1
2	Low-velocity impact failureof aluminum honeycomb sandwich panels显示文摘	Foo C C Seah L K Chai G B	2008	CompositeStructure2008，85，：	1
3	Vibration buckling of rectangularcomposite plates with variable fiber spacing 显示文摘	Leissa A W Martin A F	1990	CompositeStructures*1990，14，4：	1
4	Vibration in a satellite structure with alaminate composite hybrid sandwich panel显示文摘	Cho H K Rhee J	2011	CompositeStructures2011，93，：	1
5	Postbuckling and failure ofstiffened composite panels under axial compression 显示文摘	Kong C W Lee I C Kim C G	1998	CompositeStructures1998，42，1：	1
6	Parametric Study of the Post-bucklingStrength of Structural Core Sandwich Panels显示文摘	NORDSTRAND T M	2000	CompositeStructures2000，，30：	1
7	Numerical prediction of delamination in CFRP drilling显示文摘	FEITO N PUENTE J L SANTIUSTE C	2014	CompositeStructures2014，108，1：	1
8	Anexperimentalstudyonmatrixcrackinduceddelaminationincompositelaminates显示文摘	ZubillagaL TuronA RenartJ etal	2015	CompositeStructures2015，127，：	1
9	Buckling behavior of composite laminates with multiple delamination under uniaxial compression 显示文摘	Hwang Shunfa Liu Guihuann	2001	Compositestructures2001，53，：	1
10	StackingSequenceDesign of Composite Laminates for MaximumStrengthUsingGeneticAlgorithms显示文摘	ParkJH HwangJH LeeCS	2001	CompositeStructure2001，52，2：	1
11	Effects of joint geometry andbolt torque on the structural performance of single bolt ten-sion joints in pultruded GRP sheet material显示文摘	COOPER C TURVEY G J	1995	CompositeStructures1995，32，14：	1
12	AcomparisonbetweenMonteCarloandFORMsincalculatingthereliabilityofacom-positestructure显示文摘	SciuvaMD LomarioDA	2003	CompositeStructure2003，59，1：	1
13	Compositesandwichconstructionsforabsorbingtheelectromagneticwaves显示文摘	Kim PC LeeD G	2009	CompositeStructures2009，87，2：	1
14	Interfacial stresses in plated beams with cracks显示文摘	Yang Jian Ye J Q	2002	CompositeStructures2002，57，1：	1
15	Buckling behavior of com- posite laminates with multiple delamination under uniaxial com- pression显示文摘	Hwang Shunfa Liu Guihuann	2001	Compositestructures2001，53，：	1
16	Low temperature effect on impact response ofquasi-isotropic glass/epoxy laminated plates显示文摘	Icten B M	2009	CompositeStructures2009，91，3：	1
17	An analytical model for the prediction ofload distribution in highly torqued multi-bolt composite joints显示文摘	MCCARTHY C T GRAY P J	2011	CompositeStructures2011，，93：	1
18	Three-dimensionalfinite element analysis of single-bolt, single-lap compositebolted joints: part1-model development and validation 显示文摘	MCCARTHY M A MCCARTHY C T LAWLOR V P	2005	CompositeStructures2005，，11：	1
19	Finite element modeling and optimazation of loadtransfer in multi-fastener joints using structural element 显示文摘	JOHAN E SCHON J	2008	CompositeStructures2008，，1：	1
20	Optimum buckling design ofcomposite stiffened panels using ant colony algorithm显示文摘	Wei Wang Guo S Nan Chang	2010	CompositeStructures2010，92，3：	1

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