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97篇 您的检索式:作者名="Tserpes"
    题名 作者 年代 出处 被引量
1Adhesive bonding of composite aircraft structures:Challenges and recent developments显示文摘In this review paper,the challenges and some recent developments of adhesive bonding technology in composite aircraft structures are discussed.The durability of bonded joints is defined and presented for parameters that may influence bonding quality.Presented is also,a numerical design approach for composite joining profiles used to realize adhesive bonding.It is shown that environmental ageing and pre-bond contamination of bonding surfaces may degrade significantly fracture toughness of bonded joints.Moreover,it is obvious that additional research is needed in order to design joining profiles that will enable load transfer through shearing of the bondline.These findings,together with the limited capabilities of existing non-destructive testing techniques,can partially explain the confined use of adhesive bonding in primary composite aircraft structural parts.PANTELAKIS Sp. TSERPES K.I. 2014Science China(Physics,Mechanics & Astronomy)2014,57,1:5
2Analytical calculation of local buckling and post-buckling behavior of isotropic and orthotropic stiffened panels显示文摘D.G. Stamatelos G.N. Labeas K.I. Tserpes 2010Thin-Walled Structures2010,,3:2
3Strength prediction of bolted joints in graphite/epoxy composite laminates显示文摘K.I Tserpes G Labeas P Papanikos Th Kermanidis 2002Composites Part B2002,,7:2
4Progressive damage modeling of bonded composite repairs显示文摘Papanikos P Tserpes K I Labeas G 2005Theoretical and Ap?plied Fracture Mechanics2005,43,2:1
5Strength prediction of bolted joints in graphite/epoxy composite laminates 显示文摘Tserpes K I Labeas G Papanikos P Kermanidis T 2002Composites Part B2002,33,:1
6Multi-scale Modeling of Tensile Behavior of Carbon Nanotube-reinforeed Composites显示文摘Tserpes KI Papanikos P Labeas G 2008Theoretical and Applied Fracture Mechanics2008,49,1:1
7Strength prediction of bolted joints in graphite/epoxy composite laminates显示文摘TSERPES K I LABEAS G PAPANIKOS P 2002Composites:Part B2002,33,:1
8Stength prediction of bolted joints in graphi- te/epoxy composite laminates显示文摘 G Labeas P Papanikos T Kermanidis 2002Composites: Part B2002,33,:1
9Fatigue damage accumulation and residual strength assessment of CFRP laminates显示文摘Tserpes K I Papanikos P Labeas G 2004Composite Structures2004,65,2:1
10Modelling of fatigue damage progression and life of CFRP laminates显示文摘Papanikos P Tserpes K I Pantelakis Sp 2003Fatigue Fraet Engng Mater Struct2003,26,:1
11Strength prediction of boltedJoints in graphite/ epoxy composite laminates显示文摘Tserpes K I Labeas G 2002Composite Part B: En?gineering2002,33,7:1
12A three-dimensional progressive damage model for boltedJoints in composite lami?nates subjected to tensile loading显示文摘Tserpes K I Papanikos P Kermanidis T 2002Fatigue and Fracture of Engineering Materials and Structures2002,24,10:1
13A three dimensional progressive damage model for bolted joints in composite laminates subjected to tensile loading 显示文摘Tserpes K I Papanikos P Kermanidis T H 2002Composites Part B2002,33,1:1
14Strength prediction of bolted joints in graphite/epoxy composite laminates显示文摘Tserpes KI Labeas G Papanikos P 0,,07:1
15A three dimensional progressive damage model for bolted joints in composite laminates subjected to tensile loading显示文摘TSERPES K I PAPANIKOS P KERMANIDIS T 2001Fatigue Fracture of Engineering Materials ~ Structures2001,24,10:1
16Strength prediction of bolted joints in graphite/epoxy composite laminates显示文摘Tserpes K I Labeas G Papanikos P 2002Composites: Part B2002,33,7:1
17Strength prediction of bolted joints in graphite/epoxy composite laminates 显示文摘Tserpes K I Labeas G Papanikos P 2002Composites Part B: Engineering2002,33,7:1
18Strength prediction of bolted joints in graphite/epoxy composite laminates 显示文摘TSERPES K I LABEAS G 2002Compos B : Eng2002,33,7:1
19Mesomechanical analysis of non- crimp fabric composite structural parts显示文摘Tserpes K I Labeas G N 2009Compos Struct2009,87,:1
20Strength prediction of bolted joints in graphite/epoxy composite laminates 显示文摘TSERPES K I LABEAS G PAPANIKOS P 2002Composites: Part B2002,33,5:1
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