ir Sjoerd O van der Veen
Airbus Group NV
My co-authors include
Dr René C Alderliesten
Professor Michael Fitzpatrick
Creep behaviour of Ti-6Al-4V produced by SLM
Measurement and modelling of residual stress in wire-feed additively manufactured titanium
Materials Science and Technology
Impact of forming process on static, fatigue and damage tolerance properties
Predicting the paths of fatigue cracks in alloys with anisotropic crack resistance
Residual Fatigue Properties of a 2024-T351 Aluminium Alloy from the Teardown of AIRBUS ...
Advanced Materials Research
Novel Aerospace Architectures Made Possible by Forming Simulation
Key Engineering Materials
AK-ILS: An Active learning method based on Kriging for the Inspection of Large Surfaces
Tailoring Static Strength Performance of Metallic Stiffened Panels by Selective Local S...
Post-Buckling Failure of Welded Aluminum Panels
Stiffened Panels in Compression: Redirecting Loads Toward High-Strength Stiffeners
Prediction of Spectrum Fatigue Crack Growth in Latest Generation High Damage Tolerance ...
Optimizing New Aluminum Alloys Through Computer Simulation
Monolithic Structure: Materials and Methods for Reduced Cost, Reduced Weight and Improv...
On Material Models for Static Sizing of Compression Driven Airframe Structure