Analysis and optimisation of parameters influencing the out-of-plane energy absorption of an aluminium honeycomb

Abstract To improve the efficiency of the numerical simulation of the crushing of a honeycomb structure, the equivalent solid model of an aluminium honeycomb core was established. Comparison between the numerical simulation results and experimental evidence revealed that the numerical model of the honeycomb structure was effectively verified as representative. Secondly, the response surfaces for the variation of specific energy absorption (SEA) with side length l and thickness t of the aluminium foil were constructed by surrogate models. Then the relationship between SEA variation and the length l and thickness t of the aluminium foil was investigated. Results indicated that SEA increased with increasing t and decreased with increasing l. The optimum SEA and associated structural parameters (l=1.0 mm, and t=0.16 mm) of an aluminium honeycomb were obtained.

[1]  Saeed Maghsoodloo,et al.  Simulation optimization based on Taylor Kriging and evolutionary algorithm , 2011, Appl. Soft Comput..

[2]  H. R. Zarei,et al.  Multiobjective crashworthiness optimization of circular aluminum tubes , 2006 .

[3]  Tau Tyan,et al.  Quasi-static crush behavior of aluminum honeycomb specimens under non-proportional compression-dominant combined loads , 2006 .

[4]  Zhi-Wei Wang,et al.  Mathematical modelling of energy absorption property for paper honeycomb in various ambient humidities , 2010 .

[5]  Fatih Aruk,et al.  Railroad passenger car collision analysis and modifications for improved crashworthiness , 2011 .

[6]  Shahram Azadi,et al.  NVH analysis and improvement of a vehicle body structure using DOE method , 2009 .

[7]  Jian Chen,et al.  Optimal design of aeroengine turbine disc based on kriging surrogate models , 2011 .

[8]  L. Nilsson,et al.  On polynomial response surfaces and Kriging for use in structural optimization of crashworthiness , 2005 .

[9]  Bin Wang,et al.  Mushrooming of circular tubes under dynamic axial loading , 2002 .

[10]  Giovanni Belingardi,et al.  Material characterization of a composite–foam sandwich for the front structure of a high speed train , 2003 .

[11]  Ali Ghamarian,et al.  Crashworthiness investigation of conical and cylindrical end-capped tubes under quasi-static crash loading , 2012 .

[12]  Zhang Weihong,et al.  Mean out-of-plane dynamic plateau stresses of hexagonal honeycomb cores under impact loadings , 2010 .

[13]  Xu Han,et al.  Multiobjective optimization for tapered circular tubes , 2011 .

[14]  Guoxing Lu,et al.  Dynamic behavior of graded honeycombs - A finite element study , 2013 .

[15]  Mpf Sutcliffe,et al.  Compressive characteristics of foam-filled composite egg-box sandwich panels as energy absorbing structures , 2010 .

[16]  Xi Yang,et al.  Aerodynamic and heat transfer design optimization of internally cooling turbine blade based different surrogate models , 2011 .

[17]  Zbigniew Sekulski,et al.  Multi-objective topology and size optimization of high-speed vehicle-passenger catamaran structure by genetic algorithm , 2010 .

[18]  Qiang Li,et al.  A two-stage multi-objective optimisation of vehicle crashworthiness under frontal impact , 2008 .

[19]  Tau Tyan,et al.  Quasi-static crush behavior of aluminum honeycomb specimens under compression dominant combined loads , 2006 .

[20]  J. M. Alexander AN APPROXIMATE ANALYSIS OF THE COLLAPSE OF THIN CYLINDRICAL SHELLS UNDER AXIAL LOADING , 1960 .

[21]  Marcus Redhe,et al.  A method to determine structural sensitivities in vehicle crashworthiness design , 2002 .

[22]  Tomasz Sadowski,et al.  Effective elastic properties of foam-filled honeycomb cores of sandwich panels , 2010 .

[23]  Heung-Soo Kim,et al.  New extruded multi-cell aluminum profile for maximum crash energy absorption and weight efficiency , 2002 .

[24]  Jian-Hong Chen,et al.  Crashworthiness assessment of square aluminum extrusions considering the damage evolution , 2006 .

[25]  Vincent Caccese,et al.  Optimal Design of Honeycomb Material Used to Mitigate Head Impact. , 2013, Composite structures.

[26]  N. Fleck,et al.  Dynamic compressive response of composite square honeycombs , 2012 .

[27]  Zhang Weihong,et al.  Mean in-plane plateau stresses of hexagonal honeycomb cores under impact loadings , 2009 .

[28]  Marcus Redhe,et al.  An investigation of structural optimization in crashworthiness design using a stochastic approach , 2004 .

[29]  Ramana V. Grandhi,et al.  Two-level optimization of airframe structures using response surface approximation , 2000 .

[30]  Sultan Noman Qasem,et al.  Multi-objective hybrid evolutionary algorithms for radial basis function neural network design , 2012, Knowl. Based Syst..

[31]  Faustino Mujika,et al.  On the determination of out-of-plane elastic properties of honeycomb sandwich panels , 2011 .

[32]  Qing Li,et al.  Optimization of foam-filled bitubal structures for crashworthiness criteria , 2012 .

[33]  M. Ashby,et al.  Cellular solids: Structure & properties , 1988 .

[34]  E. Acar,et al.  Multi-objective crashworthiness optimization of tapered thin-walled tubes with axisymmetric indentations , 2011 .

[35]  I. Eren,et al.  Finite element analysis of collapse of front side rails with new types of crush initiators , 2009 .

[36]  David P. Thambiratnam,et al.  Crushing response of foam-filled conical tubes under quasi-static axial loading , 2009 .

[37]  Hui Zhou,et al.  Energy-absorption forecast of thin-walled structure by GA-BP hybrid algorithm , 2013 .

[38]  H. Zarei,et al.  Optimum honeycomb filled crash absorber design , 2008 .

[39]  Bertan Bayram,et al.  The effect of geometrical parameters on the energy absorption characteristics of thin-walled structures under axial impact loading , 2010 .

[40]  Jae-Yong Park,et al.  Reliability-based topology optimization using a standard response surface method for three-dimensional structures , 2011 .