Calvin Rans
TitleCited byYear
Misinterpreting the results: How similitude can improve our understanding of fatigue delamination growth
C Rans, R Alderliesten, R Benedictus
Composites Science and Technology 71 (2), 230-238, 2011
The applicability of magnesium based fibre metal laminates in aerospace structures
R Alderliesten, C Rans, R Benedictus
Composites Science and Technology 68 (14), 2983-2993, 2008
Riveting process induced residual stresses around solid rivets in mechanical joints
C Rans, PV Straznicky, R Alderliesten
Journal of aircraft 44 (1), 323-329, 2007
Applicability of AZ31B-H24 magnesium in fibre metal laminates–an experimental impact research
T Pärnänen, R Alderliesten, C Rans, T Brander, O Saarela
Composites Part A: Applied Science and Manufacturing 43 (9), 1578-1586, 2012
Fatigue performance of additively manufactured meta-biomaterials: The effects of topology and material type
SM Ahmadi, R Hedayati, Y Li, K Lietaert, N Tümer, A Fatemi, CD Rans, ...
Acta biomaterialia 65, 292-304, 2018
Application of a modified Wheeler model to predict fatigue crack growth in Fibre Metal Laminates under variable amplitude loading
SU Khan, RC Alderliesten, CD Rans, R Benedictus
Engineering Fracture Mechanics 77 (9), 1400-1416, 2010
The role of rivet installaton on the fatigue performance of riveted lap joints
CD Rans
Carleton University, 2007
Isolated and modulated effects of topology and material type on the mechanical properties of additively manufactured porous biomaterials
R Hedayati, SM Ahmadi, K Lietaert, B Pouran, Y Li, H Weinans, CD Rans, ...
Journal of the mechanical behavior of biomedical materials 79, 254-263, 2018
Predicting the influence of temperature on fatigue crack propagation in Fibre Metal Laminates
CD Rans, RC Alderliesten, R Benedictus
Engineering fracture mechanics 78 (10), 2193-2201, 2011
Mechanical behaviour of thermoplastic composites spot-welded and mechanically fastened joints: A preliminary comparison
T Zhao, G Palardy, IF Villegas, C Rans, M Martinez, R Benedictus
Composites Part B: Engineering 112, 224-234, 2017
Effects of applied stress ratio on the fatigue behavior of additively manufactured porous biomaterials under compressive loading
J de Krijger, C Rans, B Van Hooreweder, K Lietaert, B Pouran, ...
Journal of the mechanical behavior of biomedical materials 70, 7-16, 2017
The meaning of threshold fatigue in fibre metal laminates
R Alderliesten, C Rans
International journal of fatigue 31 (2), 213-222, 2009
Analytical prediction of Mode I stress intensity factors for cracked panels containing bonded stiffeners
C Rans, R Rodi, R Alderliesten
Engineering Fracture Mechanics 97, 12-29, 2013
Effect of stress ratio on delamination growth behavior in unidirectional carbon/epoxy under mode I fatigue loading
R Khan, CD Rans, R Benedictus, DN HS
ICCM-17 International Conferences on Composite Materials, 1-11, 2009
Assessing the effects of riveting induced residual stresses on fatigue crack behaviour in lap joints by means of fractography
CD Rans, RC Alderliesten, PV Straznicky
International journal of fatigue 31 (2), 300-308, 2009
Formulating an effective strain energy release rate for a linear elastic fracture mechanics description of delamination growth
CD Rans, RC Alderliesten
Proceedings of the 17th International Conference on Composite Materials …, 2009
Effects of rivet installation on residual stresses and secondary bending stresses in a riveted lap joint
C Rans, P Straznicky, R Alderliesten
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2007
On the onset of the asymptotic stable fracture region in the mode II fatigue delamination growth behaviour of composites
CD Rans, J Atkinson, C Li
Journal of Composite Materials 49 (6), 685-697, 2015
Characterizing fatigue delamination growth behaviour using specimens with multiple delaminations: The effect of unequal delamination lengths
JA Pascoe, CD Rans, R Benedictus
Engineering Fracture Mechanics 109, 150-160, 2013
Fatigue behavior of fiber/metal laminate panels containing internal carbon tear straps
C Rans, F Morinière, R Rodi, R Alderliesten, R Benedictus
Journal of aircraft 48 (6), 2122-2129, 2011
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