Damage-tolerance-based life prediction of aeroengine compressor discs. II, A probabilistic fracture mechanics approachKOUL, A. K; BELLINGER, N. C; GOULD, G et al.International journal of fatigue. 1990, Vol 12, Num 5, pp 388-396, issn 0142-1123, 9 p.Article

Modelling of pillowing due to corrosion in fuselage lap jointsBELLINGER, N. C; KRISHNAKUMAR, S; KOMOROWSKI, J. P et al.Canadian aeronautics and space journal. 1994, Vol 40, Num 3, pp 125-130, issn 0008-2821Article

Damage-tolerance-based life prediction of aeroengine compressor discs. I, A deterministic fracture mechanics approachKOUL, A. K; BELLINGER, N. C; FAHR, A et al.International journal of fatigue. 1990, Vol 12, Num 5, pp 379-387, issn 0142-1123, 9 p.Article

Fatigue modeling for aircraft structures containing natural exfoliation corrosionLIAO, M; RENAUD, G; BELLINGER, N. C et al.International journal of fatigue. 2007, Vol 29, Num 4, pp 677-686, issn 0142-1123, 10 p.Article

Surface property improvement in titanium alloy gas turbine components through ion implantation = Amélioration des propriétés de surface des pièces de turbine à gaz en alliage de titane par implantation ioniqueELDER, J. E; PISHVA, M. R; BELLINGER, N. C et al.AGARD conference proceedings. 1989, Num 461, pp 16.1-16.11, issn 0549-7191Conference Paper

Local stress effects of corrosion in lap splicesKOMOROWSKI, J. P; BELLINGER, N. C; GOULD, R. W et al.RTO Meeting proceedings. 1999, pp 5.1-5.8, isbn 92-837-1011-8Conference Paper

Damage tolerance implications of corrosion pillowing on fuselage lap jointsBELLINGER, N. C; KOMOROWSKI, J. P; GOULD, R. W et al.Journal of aircraft. 1998, Vol 35, Num 3, pp 487-491, issn 0021-8669Article

Service-induced damage in turbine discs and its influence on damage tolerance-based life predictionPISHVA, M. R; KOUL, A. K; BELLINGER, N. C et al.Canadian aeronautics and space journal. 1989, Vol 35, Num 1, pp 4-11, issn 0008-2821Article