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48篇 您的检索式：作者名="Kermanidis T"

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	题名	作者	年代	出处	被引量
1	Strength prediction of bolted joints in graphite/epoxy composite laminates 显示文摘	Tserpes K I Labeas G Papanikos P Kermanidis T	2002	Composites Part B2002，33，：	1
2	Understanding the effect of block overloading on the fatigue behaviour of 2024-T351 aluminium alloy using the fatigue damage map显示文摘	Rodopoulos C A Kermanidis A T	2007	International Journal of Fatigue2007，29，：	1
3	Stength prediction of bolted joints in graphi- te/epoxy composite laminates显示文摘	G Labeas P Papanikos T Kermanidis	2002	Composites: Part B2002，33，：	1
4	Numerical and experimental investigation of the laser forming process显示文摘	Kyrsanidi A K Kermanidis T B Pantelakis S G	1999	Journal of Materials Processing Technology1999，87，：	1
5	Numerical simulation of the laser welding process in butt-joint specimens显示文摘	TSIRKAS S A PAPANIKOS P KERMANIDIS T		0，，1：	1
6	Numerical simulation of laser welding process in bott-joint specimens显示文摘	Tsirkas S A Papanikos P Kermanidis T H	2003	Materials Processing Technology2003，134，：	1
7	A 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	2002	Fatigue and Fracture of Engineering Materials and Structures2002，24，10：	1
8	A 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	2002	Composites Part B2002，33，1：	1
9	A 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	2001	Fatigue Fracture of Engineering Materials ~ Structures2001，24，10：	1
10	Numerical and experimental investigation of the laser forming process 显示文摘	KYRSANIDI A K KERMANIDIS T B PANTELAKIS S G	1999	Journal of Materials Processing Technology1999，87，：	1
11	Fatigue and damage tolerance behavior of corroded 2024 T351 aircraft aluminum alloy显示文摘	KERMANIDIS A T PETROYIANNIS P V PANTELAKIS S G	2005	Theoretical and Applied Fracture Mechanics2005，43，：	1
12	Numerical simulation of laser welding process in bott-joint specimens显示文摘	Tsirkas S A Papanikos P Kermanidis T H		0，，134：	1
13	A 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	2001	Fatigue and Fracture of Engineering Materials and Structures2001，24，：	1
14	A three-dimensional progressive damage model for bolted joints in com posite laminates subjected to tensile loading 显示文摘	Tserpes K I Papanikos P Kermanidis T H	2002	Composites Part B2002，33，1：	1
15	Understanding the Effect of Block Overloading on the Fatigue Behaviour of 2024-T351 Aluminium Alloy Using the Fatigue Damage Map显示文摘	RODOPOULOS C A KERMANIDIS A T H	2007	International Journal of Fatigue2007，，29：	1
16	Fatigue and damage tolerance behaviour of corroded 2024 T351 aircraft aluminum alloy显示文摘	Kermanidis A T Petroyiannis P V Pantelakis S G	2005	Theoretical and Applied Fracture Mechanics2005，43，1：	1
17	A 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	2001	Fatigue & Fracture of Engineering Materials & Structures2001，24，10：	1
18	Strain En ergy Density Prediction of Fatigue Crack Growth from Hole of Aging Aircraft Structures显示文摘	Zuo J Z Kermanidi A T Pantelakis S G	2002	Theoretical and Applied Fracture Mechanics2002，38，：	1
19	Strength prediction of bolted joints in graphite/epoxy composite laminates显示文摘	Tserpes K I Labeas G Papanikos P Kermanidis T	2002	Composites Part B2002，33，7：	1
20	Evidence on the corrosion-induced hydrogen embrittlement of the 2024 aluminium alloy显示文摘	Petroyiannis P V Kamoutsi E Kermanidis A T	2005	Fatigue Frac Engng Mater Stmct2005，28，56：	1

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