Computational Assessment of Disbond Growth Behaviour in Adhesively Bonded Wide Joints or Patch Repairs for Primary Airframe Structures
暂无分享,去创建一个
B. Prusty | John Wang | A. Baker | G. Pearce | V. Tanulia
[1] P. Chang,et al. Experimental and Computational Assessment of Disbond Growth and Fatigue Life of Bonded Joints and Patch Repairs for Primary Airframe Structures , 2022, International Journal of Fatigue.
[2] B. Prusty,et al. A procedure to assess disbond growth and determine fatigue life of bonded joints and patch repairs for primary airframe structures , 2020 .
[3] R. Alderliesten,et al. The effect of bond-line thickness on fatigue crack growth rate in adhesively bonded joints , 2020 .
[4] A. Pirondi,et al. Improvement of a Cohesive Zone Model for Fatigue Delamination Rate Simulation , 2019, Materials.
[5] Carols G. Davila. From S-N to the Paris law with a new mixed-mode cohesive fatigue model for delamination in composites , 2018 .
[6] Albert Turon,et al. Accurate simulation of delamination under mixed-mode loading using a cohesive model with a mode-dependent penalty stiffness , 2018 .
[7] D. Mollenhauer,et al. Progressive failure simulation in laminated composites under fatigue loading by using discrete damage modeling , 2016 .
[8] Nabil M. Chowdhury,et al. Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures , 2015 .
[9] Alan Baker,et al. On the Certification of Bonded Repairs to Primary Composite Aircraft Components , 2015 .
[10] A. Pirondi,et al. Simulation of fatigue debonding in adhesively bonded threedimensional joint geometries using a cohesive zone model approach , 2013 .
[11] N. Tsouvalis,et al. A 3D ductile constitutive mixed-mode model of cohesive elements for the finite element analysis of adhesive joints , 2013 .
[12] A. Pirondi,et al. A procedure for the simulation of fatigue crack growth in adhesively bonded joints based on the cohesive zone model and different mixed-mode propagation criteria , 2011 .
[13] A. D. Crocombe,et al. Predicting fatigue damage in adhesively bonded joints using a cohesive zone model , 2010 .
[14] Stephen R Hallett,et al. A fatigue degradation law for cohesive interface elements – Development and application to composite materials , 2010 .
[15] Stephen R Hallett,et al. Cohesive zone length in numerical simulations of composite delamination , 2008 .
[16] Pedro P. Camanho,et al. Simulation of delamination in composites under high-cycle fatigue , 2007 .
[17] M. Heller,et al. Theoretical and experimental research into optimal edge taper of bonded repair patches subject to fatigue loadings , 2005 .
[18] Liyong Tong,et al. Analysis of energy release rate for fatigue cracked metal-to-metal double-lap shear joints , 2005 .
[19] Alan Baker,et al. Fatigue crack growth in adhesively bonded composite-metal double-lap joints , 2002 .
[20] A. Baker,et al. Development of a generic repair joint for certification of bonded composite repairs , 1999 .
[21] Liyong Tong,et al. A damage zone model for the failure analysis of adhesively bonded joints , 1998 .
[22] キャスリーン・エイ・マイヤー,et al. Composite aircraft structure , 1998 .
[23] S. Mall,et al. Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch , 1997 .
[24] J. Whitney,et al. Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations , 1974 .
[25] John Wang,et al. Adhesively Bonded Repair/Reinforcement of Metallic Airframe Components: Materials, Processes, Design and Proposed Through-Life Management , 2018 .
[26] Alastair Johnson,et al. Numerical modelling of impact and damage tolerance in aerospace composite structures , 2015 .
[27] A. Pirondi,et al. A Cohesive Zone Model for Three-dimensional Fatigue Debonding/Delamination , 2014 .
[28] A. Baker. Repair of metallic airframe components using fibre-reinforced polymer (FRP) composites , 2014 .
[29] R. Benedictus,et al. Fatigue Disbonding of Bonded Repairs – An Application of the Strain Energy Approach , 2013 .
[30] A. Crocombe,et al. Modelling the static response of unaged adhesively bonded structures , 2013 .
[31] P. Madelpech,et al. Bonded Composite Patch to Repair Metallic Structures: Disbond Propagation Testing and Modelling , 2009 .
[32] Peter Chalkley,et al. Fatigue Testing of Generic Bonded Joints , 2002 .
[33] M. D. Moura,et al. Mixed-Mode Decohesion Elements for Analyses of Progressive Delamination , 2001 .
[34] M. Benzeggagh,et al. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus , 1996 .
[35] A. Baker. Crack patching: experimental studies, practical applications , 1988 .