A Corrosion Damage Quantification Approach for Assessing the Tensile Behavior of Corroded Aluminum Alloy 2024
Sp.G. Pantelakis, D.D. Setsika, K.I. Tserpes. A.N. Chamos
pantelak@mech.upatras.gr; kit2005@mech.upatras.gr
Fatigue-Creep Crack Growth Characteristics of α+β Titanium Alloys: Transition of Data in Segments of Macro-Micro-Nano
G.C. Sih, K.K. Tang
zpg7463@yahoo.com
Advances in the Application of Supersonic Particle Deposition to Load Bearing Aerospace and Non-Aerospace Structures
R. Jones, N. Matthews, B. Wamsley
rhys.jones@monash.edu
Aircraft Fatigue Test Interpretation Using Quantitative Fractography
S. Barter, L. Molent
simon.barter@dsto.degebce.gov.au
Fatigue Crack Growth of Aircraft Structure: Sensitivity of Material Parameters
P.M.S.T. de Castro, S.M.O. Tavares
ptcastro@fe.up.pt
Design Implications Based on 6-DoF Multiaxial Robotic Testing for Characterization of Composites
J. Michopoulos, A. Iliopoulos, J. Hermanson
john.michopoulos@nrl.navy.mil
Advantages of the Strain Energy Density for Fracture and Fatigue Assessment of Sharp and Blunt V-Notches
F. Berto, P. Lazzarin
berto@gest.unipd.it