1. K. I. Tserpes, P. Papanikos, T. Kermanidis, A three‐dimensional progressive damage model for bolted joints in composite laminates subjected to tensile loading, Fatigue & Fracture of Engineering Materials & Structures, 24(10), pp. 663–675, (2001)
2. Al. Th. Kermanidis, Sp. G. Pantelakis, “Fatigue Crack Growth Analysis of 2024 T3 Aluminium Specimens Under Aircraft Service Spectra”, Fatigue Fract Engng Mater Struct 24, (2001), pp. 699-710
3. D. Diamantakos, G. Labeas, Sp. Pantelakis, Th. Kermanidis, “A Model to Assess the Fatigue Behaviour of Ageing Aircraft Fuselage”, Fatigue Fract Engng Mater Struct 24, (2001), pp. 677-686
4. Sp. G. Pantelakis, Em. Kyriakakis, P. Papanikos, “Non-destructive Fatigue Damage Chracterization of Laminated Thermosetting Fibrous Composites”, Fatigue Fract Engng Mater Struct 24, (2001), pp. 651-662
5. Kermanidis, Al.Th., Mitropoulos, I.A., Diamantoudis, A.Th., Tserpes, K.I.
The effect of trapped hydrogen on the mechanical properties of 2024 aircraft aluminium alloy. In: PROCEEDINGS OF THE ‘RECENT ADVANCES IN MECHANICAL ENGINEERING’ CONFERENCE, ASME International, Greek Section (Patras, September 17-20, Greece, 2001)
6. Sp. Pantelakis, Al. Kermanidis, P. Papanikos
“Mesodamage of 2024-T3 Aluminum Alloy Specimen due to Corrosion-Induced Localized Hydrogen Embrittlement”, In: CD-ROM Proc. of the Tenth International Conference on Fracture, December 2001, Hawaii
7. Al. Kermanidis, N.D. Alexopoulos, Sp.G. Pantelakis
'Fatigue Behavior of Corroded Aluminum Specimens'', In Proc of the 1st Panhellenic Conference on Metallic Materials, 29-30 November 2001, University of Thessaly, p. 128-133