Physics-informed machine learning for variable amplitude loading in fatigue crack growth Marknesse Master Thesis Background Fatigue in metallic structures is still considered a major threat to the continuing airworthiness of aircraft. Existing models to predict the
Job grade: AD 6 Internal job grade and Interagency: AD06 and above Type of position: Temporary agent Selection procedure reference: EMA/AD/11463 Job title: Regulatory & Scientific Digitalisation Project Management Specialist Talent Pool: AD06 Change, Programme and