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31篇 您的检索式：作者名="LABEAS G N"

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	题名	作者	年代	出处	被引量
1	Development and validation of a strain-based structural health monitoring system 显示文摘	Katsikeros Ch E Labeas G N	2009	Me- chanical Systems and Signal Processing2009，23，2：	1
2	Adaptative progressive damage modeling for large-scale composite structures显示文摘	Labeas G N Belesis S D Diamantakos I	2012	International Journal of Damage Mechanics2012，21，44：	1
3	Prediction of residual stresses and distortions due to laser beam welding of butt joints in pressure vessels显示文摘	MORAITIS G A LABEAS G N		0，，2：	1
4	Simulation of the electroimpulse de-icing process of aircraft wings显示文摘	Labeas G N 'Diamantakos I D Sunaric M M	2006	Journal of Aircraft2006，43，6：	1
5	Torsional Vibration of Acracked Rod by Variational Formulation and Nu- merical Analysis显示文摘	Chondros T G Labeas G N	2007	Journal of Sound and Vibra- tion2007，301，3：	1
6	Mesomechanical analysis of non- crimp fabric composite structural parts显示文摘	Tserpes K I Labeas G N	2009	Compos Struct2009，87，：	1
7	Simula- tion of the electro-lmpulse de-icing process of aircrat~ wings 显示文摘	LABEAS G N DIAMANTAKOS 1 D SUNARIC M M	2006	Journal of Aircraft2006，43，6：	1
8	Simulation of the electroimpulse de-icing process of aircmt~ wings显示文摘	Labeas G N Diamantakos I D Sunaric M M	2006	Joumal of Air- craft2006，43，6：	1
9	Residual stress and distortion calculation of laser beam welding for aluminum lap joints 显示文摘	MORAITIS G A LABEAS G N	2008	Journal of Materials Processing Technology2008，198，2：	1
10	Stress intensity factors of semi-elliptical surface cracks in pressure vessels by global-local finite element methodology显示文摘	Diamantoudis A Th Labeas G N	2005	Engineering Fracture Mechanics2005，72，9：	1
11	Simulation of the electroimpulse deicing process of aircraft wings 显示文摘	Labeas G N Diamantakos I D Sunnaric M M	2006	Journal of Aircraft Journal of Aircraft (S0021-8669)2006，43，6：	1
12	Stress intensity factors of semi-elliptical surface cracks in pressure vessels by global-local finite element methodology显示文摘	Labeas G N	2005	Engineering Fracture Mechanics2005，72，：	1
13	A model to assess the fatigue behavior of ageing aircraft fuselage显示文摘	Labeas G N Pantelakis SP G	2001	Fatigue & Fracture of Engineering Materials & Structures2001，24，：	1
14	Fatigue Crack Propagation Trajectories under Mixed-- mode Cyclic Loading 显示文摘	Pavou D G Labeas G N Vlachakis N V	2003	Engineering Structures2003，25，7：	1
15	Development and validation of a strain-based Structural Health Monitoring system显示文摘	ATSIKEROS C E LABEAS G N	2009	Mechanical Systems and Signal Processing2009，23，：	1
16	Development and validation of a strain-based structural health monitoring system显示文摘	Katsikeros Ch E Labeas G N	2009	Mechanical Systems and Signal Processing2009，23，2：	1
17	Simulation of the electroimpulse de icing process of aircraft wings显示文摘	Labeas G N Diamantakos I D Sunaric M M	2006	Journal of Aircraft2006，43，6：	1
18	Stress intensity factors of semi-elliptical surface cracks in pressure vessel by global-local finite element methodology显示文摘	Diamantoudis A Th Labeas G N	2005	Engineering Fracture Mechanics2005，72，：	1
19	Development and validation 6f a strain-based Structural Health Monitoring system 显示文摘	Katsikems C E Labeas G N	2009	MeChanical Systems and Signal Processing2009，23，2：	1
20	Thermome-chanical simulation of infrared heating diaphragm formingprocess for thermoplastic parts 显示文摘	Labeas G N Watiti V B Katsiropoulos C V	2008	Journal of Thermo-plastic Composite Materials2008，21，4：	1

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