On crack tunneling and plane-strain delamination in laminatesALDERLIESTEN, René C.International journal of fracture. 2007, Vol 148, Num 4, pp 401-414, issn 0376-9429, 14 p.Article

The meaning of threshold fatigue in fibre metal laminatesALDERLIESTEN, René; RANS, Calvin.International journal of fatigue. 2009, Vol 31, Num 2, pp 213-222, issn 0142-1123, 10 p.Article

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

'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

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

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

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

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

Fatigue crack growth history in damage tolerance design of aircraft structuresSIEGL, Jan; NEDBAL, Ivan; KUNZ, Jirí et al.International journal of fatigue. 2009, Vol 31, Num 6, pp 1062-1067, issn 0142-1123, 6 p.Conference Paper

Damage tolerance demonstration testing for the Australian F/A-18MOLENT, L; BARTER, S. A; WHITE, P et al.International journal of fatigue. 2009, Vol 31, Num 6, pp 1031-1038, issn 0142-1123, 8 p.Conference Paper

Eurofighter a safe life aircraft in the age of damage toleranceDILGER, Robert; HICKETHIER, Holger; GREENHALGH, Michael D et al.International journal of fatigue. 2009, Vol 31, Num 6, pp 1017-1023, issn 0142-1123, 7 p.Conference Paper

Fatigue, residual strength and non-destructive tests of an aging aircraft's wing detailKOSKI, K; SILJANDER, A; BÄCKSTRÖM, M et al.International journal of fatigue. 2009, Vol 31, Num 6, pp 1089-1094, issn 0142-1123, 6 p.Conference Paper

Weld residual stress effects on fatigue crack growth behaviour of aluminium alloy 2024-T351LILJEDAHL, C. D. M; BROUARD, J; ZANELLATO, O et al.International journal of fatigue. 2009, Vol 31, Num 6, pp 1081-1088, issn 0142-1123, 8 p.Conference Paper