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(41 - 60 of 93)
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Fractographic analysis of fatigue crack growth under simple variable-amplitude loading in 2024-T351 material
The tensile-mode/shear-mode transition during fatigue crack growth under flight-simulation loading
Eddy-current inspection of visible cracks in a riveted lapjoint of ARALL-material
Fatigue of aircraft structures
Fatigue crack closure, observations and technical significance
Collection of data on slope factors obtained in flight-simulation fatigue tests
Brief note on the estimation of stress concentration factors of sharp edge notches
The significance of flight-simulation fatigue tests
The effect of low sheet thicknesses on the fracture toughness of an AL-Alloy (7075-T6)
Size effect on the fatigue strength of a welded specimen (a brief note)
Crack growth in aluminium alloy sheet material under flight-simulation loading: 1. A comparison between twist and minitwist falstaff and short falstaff 2. Effect of truncating high loads
The practical and theoretical significance of small cracks: An evaluation
Comparison between empirical and calculated stress intensity factors of hole edge cracks
Fatigue crack growth of corner cracks in lug specimens
Interpolation between calculated stress-intensity factors of semi- and quarter elliptical cracks
Stress intensity factors of hole edge cracks. Comparison between one crack and two symmetric cracks
Fatigue crack growth in aluminium alloy sheet material under constant-amplitude and simplified flight-simulation loading
De ontwikkeling van Arrall met het oog op constructieve oplossingen (Stand van zaken dec. 1983)
Estimation of Kt-value by comparing different notch geometries
Brief note of the stress intensity factor of elliptical cracks
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