Aerothermoelastic analysis of lattice sandwich composite panels in supersonic airflow

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• 作者：Zhi-Guang Song ; Feng-Ming Li
• 关键词：Lattice sandwich composite panel ; Pyramidal truss core ; Triangular grid core ; Aerothermoelastic ; Supersonic airflow
• 刊名：Meccanica
• 出版年：2016
• 出版时间：April 2016
• 年：2016
• 卷：51
• 期：4
• 页码：877-891
• 全文大小：1,234 KB
• 参考文献：1.Xue ZY, Hutchinson JW (2003) Preliminary assessment of sandwich plates subject to blast loads. Int J Mech Sci 45:685–705CrossRef MATH
  2.Lu TJ (1999) Heat transfer efficiency of metal honeycombs. Int J Heat Mass Transf 42:2031–2040CrossRef MATH
  3.Hoffmann F, Lu TJ, Hodson HP (2003) Heat transfer performance of Kagome structures, Paper HX07, 8th UK national heat transfer conference, Oxford, 9–10 September 2003
  4.Kim T (2003) Fluid-flow and heat-transfer in a lattice-frame material. PhD Thesis, Department of Engineering, University of Cambridge
  5.ElRaheb M, Wagner P (1997) Transmission of sound across a truss-like periodic panel: 2D analysis. J Acoust Soc Am 102(4):2176–2183ADS CrossRef
  6.Cui XD, Zhao LM, Wang ZH, Zhao H, Fang DN (2012) Dynamic response of metallic lattice sandwich structures to impulsive loading. Int J Impact Eng 43:1–5CrossRef
  7.Ruzzene M (2004) Vibration and sound radiation of sandwich beams with honeycomb truss core. J Sound Vib 277:741–763ADS CrossRef
  8.Cielecka I, Jedrysiak J (2006) A non-asymptotic model of dynamics of honeycomb lattice-type plates. J Sound Vib 296:130–149ADS CrossRef
  9.Dharmasena KP, Wadley HNG, Williams K, Xue ZY, Hutchinson JW (2011) Response of metallic pyramidal lattice core sandwich panels to high intensity impulsive loading in air. Int J Impact Eng 38:275–289CrossRef
  10.McShane GJ, Deshpande VS, Fleck NA (2010) Underwater blast response of free-standing sandwich plates with metallic lattice cores. Int J Impact Eng 37:1138–1149CrossRef
  11.Lok TS, Cheng QH (2001) Free and forced vibration of simply supported orthotropic sandwich panel. Comput Struct 79:301–312CrossRef
  12.Lou J, Ma L, Wu LZ (2012) Free vibration analysis of simply supported sandwich beams with lattice truss core. Mater Sci Eng, B 177:1712–1716CrossRef
  13.Chattopadhyay A, Kim JS, Liu Q (2002) Aeromechanical stability analysis and control of smart composite rotor blades. J Vib Control 8:847–860CrossRef
  14.Ghoman SS, Azzouz MS (2012) Supersonic aerothermoelastic nonlinear flutter study of curved panels: time domain. J Aircraft 49(4):1179–1183
  15.Lee YS, Vakakis AF, Bergman LA, McFarland DM, Kerschen G (2007) Suppressing aeroelastic instability using broadband passive targeted energy transfers, part I: theory. AIAA J 45:693–711ADS CrossRef
  16.Kuo SY (2011) Flutter of rectangular composite plates with variable fiber pacing. Compos Struct 93:2533–2540CrossRef
  17.Dowell EH (1966) Nonlinear oscillations of a fluttering plate. AIAA J 4(7):1267–1275CrossRef
  18.Dowell EH (1967) Nonlinear oscillations of a fluttering plate II. AIAA J 5(10):1856–1862ADS CrossRef
  19.Attar P, Tang D, Dowell EH (2010) Nonlinear aeroelastic study for folding wing structures. AIAA J 48(10):2187–2195ADS CrossRef
  20.Han AD, Yang TY (1983) Nonlinear panel flutter using high-order triangular finite elements. AIAA J 21(10):1453–1460ADS CrossRef MATH
  21.Shin WH, Oh IK, Lee I (2009) Nonlinear flutter of aerothermally buckled composite shells with damping treatments. J Sound Vib 324:556–569ADS CrossRef
  22.Oh IK, Lee I (2006) Supersonic flutter suppression of piezolaminated cylindrical panels based on multifield layerwise theory. J Sound Vib 291:1186–1201ADS CrossRef
  23.Song ZG, Li FM (2012) Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate. Compos Struct 94:702–713CrossRef
  24.Song ZG, Li FM (2014) Aerothermoelastic analysis of nonlinear composite laminated panel with aerodynamic heating in hypersonic flow. Compos B 56:830–839CrossRef
  25.Li FM, Song ZG (2013) Flutter and thermal buckling control for composite laminated panels in supersonic flow. J Sound Vib 332(22):5678–5695ADS CrossRef
  26.Song ZG, Li FM (2014) Optimal locations of piezoelectric actuators and sensors for supersonic flutter control of composite laminated panels. J Vib Control 20(14):2118–2132CrossRef
  27.Song ZG, Li FM (2014) Investigations on the flutter properties of supersonic panels with different boundary conditions. Int J Dyn Control 2:346–353CrossRef
  28.Song ZG, Li FM (2014) Aeroelastic analysis and active flutter control of nonlinear lattice sandwich beams. Nonlinear Dyn 76(1):57–68MathSciNet CrossRef MATH
  29.Allen HG (1969) Analysis and design of structural sandwich panels. Pergamon, Oxford
  30.Jones RM (1975) Mechanics of composite materials. Taylor & Francis, London
  31.Queheillalt DT, Murty Y, Wadley HNG (2008) Mechanical properties of an extruded pyramidal lattice truss sandwich structure. Scripta Mater 58:76–79CrossRef
  32.Wang HX, Chung SW (2011) Equivalent elastic constants of truss core sandwich plates. J Press Vessel Technol 133:041203CrossRef
  33.Guo XY, Mei C (2006) Application of aeroelastic modes on nonlinear supersonic panel flutter at elevated temperatures. Comput Struct 84:1619–1628CrossRef
  34.Xue DY, Mei C (1993) Finite element non-linear panel-flutter with arbitrary temperature in supersonic flow. AIAA J 31:154–162ADS CrossRef MATH
  
• 作者单位：Zhi-Guang Song (1)
  Feng-Ming Li (1) (2)
  
  1. School of Astronautics, Harbin Institute of Technology, P.O. Box 137, Harbin, 150001, China
  2. College of Mechanical Engineering, Beijing University of Technology, Beijing, 100124, China
  
• 刊物类别：Physics and Astronomy
• 刊物主题：Physics
  Mechanics
  Civil Engineering
  Automotive and Aerospace Engineering and Traffic
  Mechanical Engineering
  
• 出版者：Springer Netherlands
• ISSN：1572-9648

文摘

This paper is devoted to investigate the aerothermoelastic properties of the composite sandwich panels with two- and three-dimensional lattice cores in supersonic airflow. Both the top and bottom face sheets of the sandwich panels are composite laminated panels. The two- and three-dimensional lattice cores are composed of triangular grids and pyramidal trusses, respectively. The first-order shear deformation theory is used in the structural modeling. The equivalent thermal expansion coefficients of the triangular grid are obtained by the physical and geometric relations of the deformed core only under the temperature change. The equation of motion of the structural system is formulated using the Hamilton’s principle. The supersonic piston theory is used to evaluate the aerodynamic pressure. The aerothermoelastic properties of the lattice sandwich panels are analyzed by the frequency-domain method. The influences of parameters of the lattice core on the aeroelastic stability of the sandwich panel are investigated. The aerothermoelastic properties of the sandwich composite panels with two- and three-dimensional lattice cores are compared. Some useful results are obtained from the present study.