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Results 1 to 25 of 31

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Damage Tolerance of Aircraft StructuresBENEDICTUS, Rinze; ALDERLIESTEN, René C.International journal of fatigue. 2009, Vol 31, Num 6, issn 0142-1123, 115 p.Conference Proceedings

Crack closure and fibre bridging during delamination growth in carbon fibre/epoxy laminates under mode I fatigue loadingKHAN, Rafiullah; ALDERLIESTEN, René; LIAOJUN YAO et al.Composites. Part A, Applied science and manufacturing. 2014, Vol 67, pp 201-211, issn 1359-835X, 11 p.Article

Two-parameter model for delamination growth under mode I fatigue loading (Part B: Model development)KHAN, Rafiullah; ALDERLIESTEN, René; BENEDICTUS, Rinze et al.Composites. Part A, Applied science and manufacturing. 2014, Vol 65, pp 201-210, issn 1359-835X, 10 p.Article

Formability prediction of high strength aluminum sheetsABBAS ZADPOOR, Amir; SINKE, Jos; BENEDICTUS, Rinze et al.International journal of plasticity. 2009, Vol 25, Num 12, pp 2269-2297, issn 0749-6419, 29 p.Article

'WFD' ― What is it and what's 'LOV' got to do with it?EASTIN, R.International journal of fatigue. 2009, Vol 31, Num 6, pp 1012-1016, issn 0142-1123, 5 p.Conference Paper

Damage tolerance of bonded aircraft structuresALDERLIESTEN, R. C.International journal of fatigue. 2009, Vol 31, Num 6, pp 1024-1030, issn 0142-1123, 7 p.Conference Paper

Fatigue damage in aircraft structures, not wanted, but tolerated?SCHIJVE, Jaap.International journal of fatigue. 2009, Vol 31, Num 6, pp 998-1011, issn 0142-1123, 14 p.Conference Paper

Experimental characterization of the crack-tip-opening angle in fibre metal laminatesRODI, Riccardo; ALDERLIESTEN, Rene'; BENEDICTUS, Rinze et al.Engineering fracture mechanics. 2010, Vol 77, Num 6, pp 1012-1024, issn 0013-7944, 13 p.Article

The mechanical behavior of adhesively bonded tailor-made blanksZADPOOR, Amir Abbas; SINKE, Jos; BENEDICTUS, Rinze et al.International journal of adhesion and adhesives. 2009, Vol 29, Num 5, pp 558-571, issn 0143-7496, 14 p.Article

The applicability of magnesium based Fibre Metal Laminates in aerospace structuresALDERLIESTEN, René; RANS, Calvin; BENEDICTUS, Rinze et al.Composites science and technology. 2008, Vol 68, Num 14, pp 2983-2993, issn 0266-3538, 11 p.Article

Bridging effect on mode I fatigue delamination behavior in composite laminatesLIAOJUN YAO; ALDERLIESTEN, René; MEIYING ZHAO et al.Composites. Part A, Applied science and manufacturing. 2014, Vol 63, pp 103-109, issn 1359-835X, 7 p.Article

Misinterpreting the results: How similitude can improve our understanding of fatigue delamination growthRANS, Calvin; ALDERLIESTEN, René; BENEDICTUS, Rinze et al.Composites science and technology. 2011, Vol 71, Num 2, pp 230-238, issn 0266-3538, 9 p.Article

Two-parameter model for delamination growth under mode I fatigue loading (Part A: Experimental study)KHAN, Rafiullah; ALDERLIESTEN, René; BENEDICTUS, Rinze et al.Composites. Part A, Applied science and manufacturing. 2014, Vol 65, pp 192-200, issn 1359-835X, 9 p.Article

Global and Local Mechanical Properties and Microstructure of Friction Stir Welds with Dissimilar Materials and/or ThicknessesAMIR ABBAS ZADPOOR; SINKE, Jos; BENEDICTUS, Rinze et al.Metallurgical and materials transactions. A, Physical metallurgy and materials science. 2010, Vol 41, Num 13, pp 3365-3378, issn 1073-5623, 14 p.Article

Modelling cyclic shear deformation of fibre/epoxy layers in fibre metal laminatesALDERLIESTEN, René; CAMPOLI, Gianni; BENEDICTUS, Rinze et al.Composites science and technology. 2007, Vol 67, Num 11-12, pp 2545-2555, issn 0266-3538, 11 p.Article

Mechanical properties and microstructure of friction stir welded tailor-made blanksABBAS ZADPOOR, Amir; SINKE, Jos; BENEDICTUS, Rinze et al.Materials science & engineering. A, Structural materials : properties, microstructure and processing. 2008, Vol 494, Num 1-2, pp 281-290, issn 0921-5093, 10 p.Article

Fatigue Behavior of Fiber/Metal Laminate Panels Containing Internal Carbon Tear StrapsRANS, Calvin; MORINIERE, Freddy; RODI, Riccardo et al.Journal of aircraft. 2011, Vol 48, Num 6, pp 2122-2129, issn 0021-8669, 8 p.Article

Problems of laboratory tests for durability evaluation of full-scale structuresTERADA, Hiroyuki; OKADA, Takao.International journal of fatigue. 2009, Vol 31, Num 6, pp 1068-1072, issn 0142-1123, 5 p.Conference Paper

Application of Damage Tolerance principles to the design of helicoptersLAZZERI, L; MARIANI, U.International journal of fatigue. 2009, Vol 31, Num 6, pp 1039-1045, issn 0142-1123, 7 p.Conference Paper

Damage tolerance analysis of a helicopter componentTIONG, U. H; JONES, R.International journal of fatigue. 2009, Vol 31, Num 6, pp 1046-1053, issn 0142-1123, 8 p.Conference Paper

Certification programme of airframe primary structure composite part with environmental simulationRUZEK, R; BEHAL, J.International journal of fatigue. 2009, Vol 31, Num 6, pp 1073-1080, issn 0142-1123, 8 p.Conference Paper

Lamb wave detection in prepreg composite materials with fibre Bragg grating sensorsMIESEN, Nick; MIZUTANI, Yoshihiro; GROVES, Roger M et al.Proceedings of SPIE, the International Society for Optical Engineering. 2011, Vol 7981, issn 0277-786X, isbn 978-0-8194-8543-4, 79812J.1-79812J.11, 2Conference Paper

Determination of the fatigue crack-growth rate from the fractographic analysis of a specimen representing the aircraft wing skinCIESIELSKI, Marcin; KANIOWSKI, Jerzy; KARLINSKI, Wlodzimierz et al.International journal of fatigue. 2009, Vol 31, Num 6, pp 1102-1109, issn 0142-1123, 8 p.Conference Paper

Comparison of different setups for fatigue testing of thin composite laminates in bendingDE BAERE, I; VAN PAEPEGEM, W; DEGRIECLC, J et al.International journal of fatigue. 2009, Vol 31, Num 6, pp 1095-1101, issn 0142-1123, 7 p.Conference Paper

Ensuring structural damage tolerance of russian aircraftNESTERENKO, G. I; NESTERENKO, B. G.International journal of fatigue. 2009, Vol 31, Num 6, pp 1054-1061, issn 0142-1123, 8 p.Conference Paper

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