Analysis of residual strength of stiffened panels with multiple site damage

Dynamically loaded aerospace structures

Damage tolerance analyses of bolt/nut assemblies

Results of tests to be used for verification of advanced crack growth prediction models

Recent advances in the modelling of fatigue crack growth

A stripyield model including effects of hold periods at constant load

A development plan for determination of the load transfer and the stress intensity distribution in metric bolts containing a fatigue crack

Improvement of the "corpus" crack opening model in the "ESA crack" software for damage tolerance analyses: Task report 2.1, Model development

Prediction of fatigue crack growth including effects of accelerated and retarded crack propagation

Crack growth under sustained loads in aerospace materials

Prediction of low and high crack growth rates under constant and variable amplitude loading

Prediction of fatigue crack growth

Results of verification of crack growth models (Work package 7 of ESA contract 5826/84/NL/PB(SC))

Criteria for determination of significant load cycles in variable amplitude load sequences

Analysis of crack opening behaviour by application of a discretised strip yield model

A verification plan for crack growth prediction methods

Finite element analyses of stable crack growh in thin sheet material

Crack growth prediction methods: part II: selection

Crack growth prediction methods: part I: a survey

New analytical methods for the prediction of fatigue crack growth under realistic loading