Experimental and numerical analysis of the shear nonlinear behaviour of Nomex honeycomb core: Application to insert sizing

This work is a contribution to the understanding of the nonlinear shear behaviour caused by cell postbuckling in Nomex honeycomb cores. First, an experimental benchmark study was made of different designs for the shear testing of honeycomb cores. Then, several test specimens were fabricated and tested, a 3D DIC system being used to measure and record the displacements. An Artificial Neural Network (ANN) was also used to identify the onset of bucking and collapse of the cells. The influence of the overall boundary conditions of shear tests on the buckling of the cells is presented both experimentally and numerically. The reversibility and test procedure results suggest that it may be possible to allow the shear strength to be increased by up to 35% under certain conditions.

[1]  Ole Thybo Thomsen,et al.  Sandwich Plates with "Through-the-Thickness" and "Fully-Potted" inserts: Evaluation of Differences in Structural Performance , 1997 .

[2]  Steven Marguet,et al.  Modeling of Nomex® Honeycomb Cores, Linear and Nonlinear Behaviors , 2007 .

[3]  Bruno Castanié,et al.  Non-linear finite element analysis of inserts in composite sandwich structures , 2008 .

[4]  Lin-zhi Wu,et al.  Transverse shear modulus and strength of honeycomb cores , 2008 .

[5]  Gin Boay Chai,et al.  Mechanical properties of Nomex material and Nomex honeycomb structure , 2007 .

[6]  R. Das,et al.  Response of Honeycombs Subjected to In-Plane Shear , 2016 .

[7]  Ole Thybo Thomsen,et al.  Local effects in the vicinity of inserts in sandwich panels , 2004 .

[8]  M. Giglio,et al.  Numerical investigation of a three point bending test on sandwich panels with aluminum skins and Nomex™ honeycomb core , 2012 .

[9]  Yulfian Aminanda,et al.  Modelling of low-energy/low-velocity impact on Nomex honeycomb sandwich structures with metallic skins , 2008 .

[10]  Steven Marguet,et al.  Modeling of Impacts on Sandwich Structures , 2012 .

[11]  Bruno Castanié,et al.  Dynamic failure of composite and sandwich structures , 2013 .

[12]  Michel Grédiac,et al.  A finite element study of the transverse shear in honeycomb cores , 1993 .

[13]  D. Zenkert,et al.  Handbook of Sandwich Construction , 1997 .

[14]  G. Aglietti,et al.  Static and Fatigue Behaviour of Hexagonal Honeycomb Cores under In-plane Shear Loads , 2012, Applied Composite Materials.

[15]  Jin-Hwe Kweon,et al.  Testing and modeling of Nomex™ honeycomb sandwich Panels with bolt insert , 2014 .

[16]  Y. Tsujii,et al.  Analysis of Mechanical Properties of Aramid Honeycomb Core. Investigation on the Compression Strength and the Shear Modulus. , 1995 .

[18]  B. Castanié,et al.  Experimental Analysis and Modeling of the Crushing of Honeycomb Cores , 2005 .

[19]  B. Castanié,et al.  An Experimental-Numerical Approach of the Metallic Insert in CFRP/Honeycomb Sandwich Structures under Normal Tensile Load , 2011 .

[20]  Jin-Hwe Kweon,et al.  An experimental study of the insert joint strength of composite sandwich structures , 2008 .

[21]  Jin-Hwe Kweon,et al.  Characterization of Nomex honeycomb core constituent material mechanical properties , 2014 .

[22]  Christophe Bouvet,et al.  Validation and Modeling of Aeronautical Composite Structures Subjected to Combined Loadings: the VERTEX Project. Part 1: Experimental Setup, FE-DIC Instrumentation and Procedures , 2017 .

[23]  Yulfian Aminanda,et al.  Core crush criterion to determine the strength of sandwich composite structures subjected to compression after impact , 2008 .

[24]  Michael F. Ashby,et al.  The out-of-plane properties of honeycombs , 1992 .

[25]  Christophe Bouvet,et al.  Validation and modeling of aeronautical composite structures subjected to combined loadings: The VERTEX project. Part 2: Load envelopes for the assessment of panels with large notches , 2017 .

[26]  Qiran Sun,et al.  Response of aramid honeycomb sandwich panels subjected to intense impulse loading by Mylar flyer , 2017 .

[27]  Linzhi Wu,et al.  Longitudinal shear strength and failure process of honeycomb cores , 2006 .

[28]  Marco Giglio,et al.  Investigations on sandwich core properties through an experimental–numerical approach , 2012 .

[29]  Alastair Johnson,et al.  Mechanical tests for foldcore base material properties , 2009 .

[30]  Phacharaporn Bunyawanichakul Contribution à l'étude du comportement des inserts dans les structures sandwichs composites , 2005 .

[31]  B. Castanié,et al.  Experimental and Numerical Analysis of Inserts in Sandwich Structures , 2005 .

[32]  Christophe Bouvet,et al.  Experimental analysis of impact and post-impact behaviour of inserts in Carbon sandwich structures , 2019 .

[33]  T N Bitzer,et al.  Honeycomb Technology: Materials, Design, Manufacturing, Applications and Testing , 1997 .

[34]  Sebastian Heimbs,et al.  Failure behaviour of honeycomb sandwich corner joints and inserts , 2009 .

[35]  Enboa Wu,et al.  AXIAL CRUSH OF METALLIC HONEYCOMBS , 1997 .

[36]  Dieter Krause,et al.  Numerical modelling of Nomex honeycomb sandwich cores at meso-scale level , 2017 .

[37]  S. Tsai,et al.  Composite Materials: Design and Applications , 2002 .

[38]  Tomasz Wierzbicki,et al.  Crushing analysis of metal honeycombs , 1983 .

[39]  Sebastian Heimbs,et al.  Virtual testing of sandwich core structures using dynamic finite element simulations , 2009 .

[40]  Mc Farland,et al.  HEXAGONAL CELL STRUCTURES UNDER POST-BUCKLING AXIAL LOAD , 1963 .

[41]  Alastair Johnson,et al.  Numerical modelling of honeycomb core crush behaviour , 2008 .

[42]  Christos Kassapoglou,et al.  Design and Analysis of Composite Structures: With Applications to Aerospace Structures , 2010 .

[43]  Dai-heng Chen,et al.  Analysis of in-plane elastic modulus for a hexagonal honeycomb core: Effect of core height and proposed analytical method , 2009 .

[44]  Steven Marguet,et al.  An adaptive model reduction strategy for post-buckling analysis of stiffened structures , 2013 .