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A

Al.Th. Kermanidis

University of Patras

6H指数
17论文数
223被引数
收录论文 6
发表时间
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A critical consideration for the use of Al-cladding for protecting aircraft aluminum alloy 2024 against corrosion
errTHEORETICAL AND APPLIED FRACTURE MECHANICS
IF5.6
err2012-02-01
err31
PREAI
errPantelakis, Sp. G.; Chamos, A. N.; Kermanidis, Al. Th.
err分享
err收藏
Fatigue crack growth analysis of 2024 T3 aluminium specimens under aircraft service spectra
errFATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES
IF3.2
err2008-07-07
err24
PREAI
errKermanidis, AT; Pantelakis, SG
err分享
err收藏
Tensile behaviour of corroded and hydrogen embrittled 2024 T351 aluminum alloy specimen
errTHEORETICAL AND APPLIED FRACTURE MECHANICS
IF5.6
err2006-04-01
err12
PREAI
errKermanidis, Al. Th.; Stamatelos, D. G.; Labeas, G. N.; Pantelakis, Sp. G.
err分享
err收藏
Evidence on the corrosion-induced hydrogen embrittlement of the 2024 aluminium alloy
errFATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES
IF3.2
err2005-05-05
err41
PREAI
errPetroyiannis, PV; Kamoutsi, E; Kermanidis, AT; Pantelakis, SG; Bontozoglou, V; Haidemenopoulos, GN
err分享
err收藏
Fatigue and damage tolerance behaviour of corroded 2024 T351 aircraft aluminum alloy腐蚀2024 T351飞机铝合金的乏力和损伤容限行为
errTHEORETICAL AND APPLIED FRACTURE MECHANICS
IF5.6
err2005-03-01
err70
PREAI
errKermanidis, AT; Petroyiannis, PV; Pantelakis, SG
err分享
err收藏
Strain energy density prediction of fatigue crack growth from hole of aging aircraft structures
errTHEORETICAL AND APPLIED FRACTURE MECHANICS
IF5.6
err2002-07-01
err23
PREAI
errZuo, JZ; Kermanidis, AT; Pantelakis, SG
err分享
err收藏

研究方向

暂时未获取到该数据
合作学者
合作期刊
G
Gregory N. Haidemenopoulos
H 指数: 28 · 论文数: 150
G
G. Labeas
H 指数: 25 · 论文数: 100
A
A.N. Chamos
H 指数: 11 · 论文数: 26
D
Dimitrios G. Stamatelos
H 指数: 8 · 论文数: 19
Z
Zuo, JZ
H 指数: 0 · 论文数: 1
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