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69篇 您的检索式：作者名="Pantelakis"

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	题名	作者	年代	出处	被引量
1	Adhesive 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.	2014	Science China(Physics,Mechanics & Astronomy)2014，57，1：	5
2	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
3	Me- chanical performance evaluation of cast magnesium alloys for automotive and aeronautical applications显示文摘	Pantelakis S P G Alexopoulos N D Chamos A N	2007	Journal of En- gineering Materials and Technology2007，129，3：	1
4	Modelling of fatigue damage progression and life of CFRP laminates显示文摘	Papanikos P Tserpes K I Pantelakis Sp	2003	Fatigue Fraet Engng Mater Struct2003，26，：	1
5	Numerical and experimental investigation of the laser forming process显示文摘	An.K. Kyrsanidi Th.B. Kermanidis Sp.G. Pantelakis	1999	Journal of Materials Processing Tech1999，，1：	1
6	An analytical model for the prediction of distortions caused by the laser forming process 显示文摘	Kyrsanidi An K Kermanidis Th B Pantelakis Sp G	2000	Journal of Materials Processing Technology2000，104，1：	1
7	Creep resistance of aluminum alloys for the next generation supersonic civil aircrafts显示文摘	KYRSANIDI A	1999	Theoretical and Applied Fracture Mechanics1999，31，：	1
8	Creep resistance of aluminum alloys for the next generation supersonic civil aircrafts显示文摘	PANTELAKIS S KYRSAN ID IA	1999	Theoretical and Applied Fracture Mechanics1999，31，：	1
9	Hot forming behavior of non-crimp fabric PEEK/C thermoplastic composites 显示文摘	Meyer B C Katsiropoulos C V Pantelakis S G	2009	Composite Structures2009，90，2：	1
10	Tensile andenergy density properties of 2024, 6013, 8090 and 2091 aircraft aluminum alloy after corrosion exposure显示文摘	Pantelakis S G Daglaras P G Apostolopoulos C A	2000	Theoretical and Applied Fracture Mechan- ics2000，33，2：	1
11	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
12	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
13	Mechanical performance evaluation of cast magnesium alloys for automotive and aeronautical applications显示文摘	PANTELAKIS S G ALEXOPOULOS N D CHAMOS A N	2007	J Eng Mater Technol2007，129，3：	1
14	Optimization of the diaphragm forming process with regard to product quality and cost 显示文摘	Pantelakis S G Baxevani E A	2002	Composites Part A : Applied Science and Manufacturing2002，33，4：	1
15	Creep resistance of aluminium alloys for the next generation supersonic civil transport aircrafts显示文摘	Pantelakis S P Kyrsanidi A N	1999	Theretical and Applied Fracture Mechanics1999，31，：	1
16	The Effect of ultrasonic impact treatment on the fatigue resistance of friction stir welded panels显示文摘	RODOPOULOS C A PANTELAKIS S G PAPADOPOULOS M P	2009	Journal of MaterialsEngineering and Performance2009，18，9：	1
17	Creep resistance of aluminum alloys for the next generation supersonic civil aircrafts显示文摘	PANTELAKIS S KYRSANIDI A	1999	Theoretical and Applied Fracture Mechanics1999，31，：	1
18	Quality evaluation ofA357 cast aluminum alloy specimens subjected to different artificial aging treatment显示文摘	Alexopoulos N D Pantelakis S G	2004	Materials and Design2004，25，5：	1
19	Fatigue and damage tolerance behavior of corroded 2024 T351 aircraft aluminum alloy 显示文摘	KERMANIDIS AL TH PETROYIANNIS P V PANTELAKIS SP G	2005	Theoretical and Applied Fracture Mechanics2005，43，：	1
20	Optimization of the diaphragm forming process with regard to product quality and cost 显示文摘	PANTELAKIS S G BAXEVANI E A	2002	Composites Part A: @plied Science and Manufacturing (Incorporating Composites and Composites Manufacturing)2002，33，4：	1

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