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Some tests on the effect of the environment on the propagation of fatigue cracks in aluminium alloysHartman, A. (author), Jacobs, F.A. (author), Nederveen, A. (author), de Rijk, P. (author)The investigation on the propagation of fatigue cracks in aluminium alloy sheet under fluctuating tension comprised four parts. (1) Tests to determine the combined effects of the humidity of the air and the lead frequency (clad 2024-T3 and 7075-T6). (2) Tests to determine the effect of water. (3) Tests to determine the effect of wetting with a...report 1967
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- Hartman, A. (author), Jacobs, F.A. (author), van der Vet, W.J. (author) report 1965
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Hartman, A. (author), Jacobs, F.A. (author), van der Vet, W.J. (author)Several single lap Joints in clad 2024-T3 and 7075-T6 alitainium alloy with two rows of rivets or Huclcbolts have been evaluated in respect of their fatigue strength properties, both in tests with constant load amplitude and in tests with a programmed load sequence based on a gust spectrum. The results showed that: 1) The replacement of...report 1965
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Hartman, A. (author), Jacobs, F.A. (author)The propagation has been studied of fatigue cracks in 2024-T3 alclad sheet under fluctuating tension in different atmospheres. Of the principal constituents of air water vapour had a much more severe effect than oxygen; in wet -pure argon the endurance was much shorter than in dry pure oxygen. In air, other circumstances remaining unaltered, the...report 1964
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Hartman, A. (author), Jacobs, P.A. (author)A comparison has been made between the fatigue strength at fluctuating tension of 2024-T3 alclad double row riveted single lap joints at room temperature in the as fabricated condition and at 150°C after stress-aging at this temperature for 100 hours. The tests showed an appreciable decrease in endurance of the specimens tested at 150°C,...report 1963
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Hartman, A. (author), Jacobs, F.A. (author), de Rijk, P. (author)Fatigue tests on 2024-T4 alclad double row riveted single lap joints at fluctuating tension with a mean stress in the nett section of 9.0 kg/mm2 and stress amplitudes ranging from 8.6 to 3.0 kg/mm^ did not show any significant difference in endurance of similar specimens with a size ratio li2,66.report 1962