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Korswagen, Paul A. (author), Meulman, E. (author), Mariani, V. (author)
report 2018
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Korswagen, Paul A. (author), Longo, M. (author), Meulman, E. (author), van Hoogdalem, C.A. (author)
report 2017
document
Schijve, J. (author), Jacons, F.A. (author), Meulman, A.E. (author)
Flight simulation tests on 2024-T3 and 7075-T6 lug specimens indicated significant fatigue life improvements obtained by expanding the holes in accordance with the split-sleeve cold work method. Geometrical distortions induced by the expansion were measured. The significance of residual stresses is analysed with reference to depth of penetration...
report 1978
document
Schra, L. (author), van Leeuwen, H.P. (author), Meulman, A.E. (author)
The fatigue crack propagation performance of the alloy AZ 74.61 under manoeuvre spectrum loading was studied. The crack propagation behaviour was also compared with that of the American forging alloy AA 7050, not only for simulated manoeuvre loading but also for simulated gust loading and programme loading. It was found that, at comparable...
report 1976
document
Wanhill, R.J.H. (author), Meulman, A.E. (author), van der Vet, W.J. (author)
report 1974
document
van Leeuwen, H.P. (author), Schra, L. (author), Meulman, A.E. (author)
Fatigue cracks were grown in rectangular specimens with a central notch. At a certain crack length, the crack was repaired, using a variety of methods. Fatigue loading was resumed and re-initiation and subsequent growth of the fatigue crack were studied. The repair methods evaluated comprised simple stopholes, brazed straps across the crack,...
report 1970
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