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van Son, Liam (author), Arkhipov-Goyal, Amit (author), Van den Berghe, K.B.J. (author), den Ouden, Bert (author), van Vliet, Robert-Jan (author), Jacobs, Wouter (author)
report 2023
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Dejean, E.E. (author), Jacobs, J.F. (author), Den Hollander, M. (author), Oudshoorn, A. (author), Tromp, S.A. (author)
report 2003
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Roelvink, J.A. (author), Stolker, C. (author), Jacobs, C. (author)
report 2003
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Ebbens, K.W. (author), Van Wijk, M.J. (author), Slaats, M.F.L. (author), Jacobs, M.J. (author)
report 1999
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Delil, A.A.M. (author), Heemskerk, J.F. (author), Mastenbroek, O. (author), Pauw, A. (author), van Put, P.A.G. (author), Voeten, R.G.H.M. (author), Jacobs, R.H.M. (author), Muller, R. (author), Ebeling, W.D. (author), Beckmann, M.M. (author)
Capillary pumped two-phase systems are considered to be: -Prime candidates to provide efficient thermal management systems for future advanced spacecraft. -Promising candidates for the thermal control of advanced larger instruments (e.g. laser-based earth observation instruments) or microgravity experiments. In such capillary pumped two-phase...
report 1996
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Jacobs, J.B. (author), Van Rossen, J.C.P. (author)
report 1995
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Jacobs, D. (author), den Hartog, P. (author), Kuijper, J. (author)
report 1992
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Jacobs, A.A.M. (author), Van der Jagt, M.H. (author)
Document(en) uit de collectie Chemische Procestechnologie
report 1990
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Dancy, R. (author), Jacobs, D. (author)
report 1988
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Whitbread, R.E. (author), Jacobs, R.B. (author)
report 1986
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Schijve, J. (author), Jacobs, F.A. (author)
Fatigue tests were carried out on Redux and FM 123/5 bonded specimens at various stress levels, temperatures (RT to 65 C) and low and high test frequencies. Observations were made on the type of failure (bond line failure or sheet failure) and the significance of the adhesive squeezeout for crack nucleation. An analysis of the data and a...
report 1984
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Schijve, J. (author), Jacobs, F.A. (author)
Several simple crack stopping methods were evaluated In fatigue crack propagation tests on 2024-T3 Alclad sheet specimens. After precracklng until a crack of 40 mm was obtained crack stoppers were Installed and the fatigue test was continued. Crack stoppers Installed In stop holes were: a blind rivet, a hard driven rivet, a heavily tightened...
report 1984
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Jacobs, F.A. (author)
Some recent developments of the masts and standing rigging of racing-yachts and, on the other hand, the failures of a number of masts and rudderstocks led to the application of aeronautical engineering. Load spectra of the standing rigging of a 10.00 m racing yacht are given and the application of them in a lug. Some information is given on...
report 1983
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Jacobs, A.W.C.M. (author), Jacobs, W.A. (author)
Document uit de collectie Chemische Procestechnologie
report 1980
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Schijve, J. (author), Jacobs, F.A. (author), Tromp, P.J. (author)
Comparative flight-simulation tests on four types of joints of 2024- T3 sheet material were carried out with and without application of the penetrant LPS-3. Types of joints were douhle strap joint with hi-lok bolts, asymmetric strap joint, lap joint with countersunk rivets and lap joint with dimpled holes. Observations on slip during the fatigue...
report 1977
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Jacobs, F.A. (author), Schijve, J. (author), Tromp, P.J. (author)
Fatigue tests under flight-simulation loading have been performed on unnotched Alclad 2024-T3, anodised 2.0 mm thick sheet specimens, manufactured according to several machine-shop processes applied in the air craft industry. From the results it appears that milling is preferable to stamping. Rounding off the edges is also advantageous. The...
report 1977
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Wanhill, R.J.H. (author), Jacobs, F.A. (author), Schra, L. (author)
report 1976
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Schijve, J. (author), Jacobs, F.A. (author), Tromp, P.J. (author)
Flight-simulation tests based on a standardized gust load spectrum were carried out in normal air, very dry air and salt water. Specimen thicknesses were t = 2 mm and t = 10 mm, mean stress in flight was 70 or 55 MN/m². In all cases a significant effect of the environment was found. Fatigue lives for t = 10 ram were much shorter than for t = 2...
report 1976
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Schijve, J. (author), Jacobs, F.A. (author), Tromp, P.J. (author)
Flight-simulation tests were carried out on sheet specimens notched "by an open hole (Kt = 2.66). The material was 2024-T3 in three conditions; Alclad, bare and chemically milled. The crack initiation period and the crack propagation period were considerably shorter for the Alclad material. The significance of the cladding, both for constant...
report 1976
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Wanhill, R.J.H. (author), Schijve, J. (author), Jacobs, F.A. (author), Schra, L. (author)
The following text is given in the format required for presentation at the Conference and Exhibition "Fatigue Testing and Design", to be held in the City University, London, 5-9 April 1976. The report gives a comparison between the fatigue performances of several sheet and forging materials under gust spectrum loading representing the lower wing...
report 1975
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