On the progressive fatigue failure of mechanical composite joints: Numerical simulation and experimental validation

被引:25
作者
Gerendt, Christian [1 ]
Dean, Aamir [1 ]
Mahrholz, Thorsten [2 ]
Englisch, Nils [3 ]
Krause, Stefan [3 ]
Rolfes, Raimund [1 ]
机构
[1] Leibniz Univ Hannover, Inst Struct Anal, Appelstr 9A, D-30167 Hannover, Germany
[2] German Aerosp Ctr DLR, Inst Composite Struct & Adapt Syst, Lilienthalpl 7, D-738108 Braunschweig, Germany
[3] Fraunhofer Soc, Fraunhofer Inst Wind Energy Syst, Fraunhofer IWES, Seedeich 45, D-27572 Bremerhaven, Germany
关键词
Mechanical joints; Fiber reinforced polymers; Continuum damage modeling; Progressive fatigue damage prediction; Experimental validation; FIBER-REINFORCED PLASTICS; REVEALING COMPLEX ASPECTS; BOLTED JOINTS; DAMAGE MODEL; PART II; COMPRESSIVE FAILURE; POLYMER COMPOSITES; SPECTRUM FATIGUE; BEARING FAILURE; CFRP COMPOSITE;
D O I
10.1016/j.compstruct.2020.112488
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this study, a novel holistic progressive damage model for mechanical fiber-reinforced polymer (FRP) joints under static and fatigue loading is presented. The model is implemented as a user-defined subroutine in the finite element software ABAQUS/Implicit. First, the theoretical basis of both the static and the fatigue damage model are explained in detail. Here, special emphasis is put on the introduction of the FRP fatigue damage model (FDM), which is based on a physically-motivated hypothesis enabling the consistent coupling of static and fatigue damage properties. Furthermore, detailed insights concerning the experimental calibration of the FDM are presented for the first-time. Subsequently, the presented damage model is validated using first-hand experimental results for standard bolt bearing, as well as T-bolt bearing, test setups. The experimental bearing setups are tested and analyzed until ultimate failure, applying static and fatigue loading. It is shown that the model prognoses are in close accordance with experimental measurements and observations in terms of static joint strength, cyclic stiffness degradation and cycles to failure. The rich information provided by the damage model concerning the progressive damage evolution under static and fatigue loading conditions allows for its application within virtual test rigs for mechanical FRP joints. In that context, this work demonstrates the promising abilities and features of the energy hypothesis applied for the FDM for use-cases of significant rel-evance in the composite industry for the first time in literature.
引用
收藏
页数:20
相关论文
共 63 条
[1]  
Airbus, 2013, 10009 AITM
[2]  
Alderliesten R, 2017, SOLID MECH APPL, V236, P1, DOI 10.1007/978-3-319-56227-8
[3]   Revealing complex aspects of compressive failure of polymer composites - Part II: Failure interactions in multidirectional laminates and validation [J].
Bishara, M. ;
Vogler, M. ;
Rolfes, R. .
COMPOSITE STRUCTURES, 2017, 169 :116-128
[4]   Revealing complex aspects of compressive failure of polymer composites - Part I: Fiber kinking at microscale [J].
Bishara, M. ;
Rolfes, R. ;
Allix, O. .
COMPOSITE STRUCTURES, 2017, 169 :105-115
[5]   Numerical modelling and simulation of fatigue damage in carbon fibre reinforced plastics at different stress ratios [J].
Brod, M. ;
Just, G. ;
Dean, A. ;
Jansen, E. ;
Koch, I ;
Rolfes, R. ;
Gude, M. .
THIN-WALLED STRUCTURES, 2019, 139 :219-231
[6]  
Camanho P, 2011, COMPOSITE JOINTS AND CONNECTIONS: PRINCIPLES, MODELLING AND TESTING, P1, DOI 10.1533/9780857094926
[7]   Hybrid titanium-CFRP laminates for high-performance bolted joints [J].
Camanho, P. P. ;
Fink, A. ;
Obst, A. ;
Pimenta, S. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2009, 40 (12) :1826-1837
[8]   A progressive damage model for mechanically fastened joints in composite laminates [J].
Camanho, PP ;
Matthews, FL .
JOURNAL OF COMPOSITE MATERIALS, 1999, 33 (24) :2248-2280
[9]   A simulation method for fatigue-driven delamination in layered structures involving non-negligible fracture process zones and arbitrarily shaped crack fronts [J].
Carreras, L. ;
Turon, A. ;
Bak, B. L. V. ;
Lindgaard, E. ;
Renart, J. ;
Martin de la Escalera, F. ;
Essa, Y. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2019, 122 :107-119
[10]   Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures [J].
Chowdhury, Nabil ;
Chiu, Wing Kong ;
Wang, John ;
Chang, Paul .
COMPOSITE STRUCTURES, 2015, 121 :315-323