Computational analysis of failure mechanisms in composite sandwich space structures subject to cyclic thermal loading
Accurate prediction of the thermal stability and durability of composite sandwich materials used in space structures remains a challenge due to the variability of thermal related material coefficients at different temperatures and the extensive use of adhesively bonded joint fittings. This paper pre...
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| Published in | Composite structures Vol. 256; p. 113086 |
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| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Ltd
15.01.2021
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| Subjects | |
| Online Access | Get full text |
| ISSN | 0263-8223 1879-1085 |
| DOI | 10.1016/j.compstruct.2020.113086 |
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| Abstract | Accurate prediction of the thermal stability and durability of composite sandwich materials used in space structures remains a challenge due to the variability of thermal related material coefficients at different temperatures and the extensive use of adhesively bonded joint fittings. This paper presents an investigation into the thermomechanical performance of complex honeycomb core composite sandwich structures with bonded fittings exposed to extreme temperature ranges. First, detailed analyses are conducted to investigate the failure and predict the intrinsic nonlinear material properties of a specific aerospace-grade aluminum honeycomb core and carbon-epoxy composite face sheet. Sandwich panels with two types of bonded fittings are chosen to investigate nonlinear effects such as shear buckling and plastic deformation in the honeycomb core, and the progressive damage response in composite skins under different loading conditions. The nonlinear properties and modeling strategies are then incorporated in the subsequent analysis of a spacecraft’s thrust tube sandwich structure subject to cyclic thermal loading. The predicted damage and failure in the thrust tube section with an adhesively bonded cup fitting correlated with experimental observations. The current methodology offers a consistent technique for investigating the thermomechanical performance of sandwich structures with other configurations of bonded joints and fittings. |
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| AbstractList | Accurate prediction of the thermal stability and durability of composite sandwich materials used in space structures remains a challenge due to the variability of thermal related material coefficients at different temperatures and the extensive use of adhesively bonded joint fittings. This paper presents an investigation into the thermomechanical performance of complex honeycomb core composite sandwich structures with bonded fittings exposed to extreme temperature ranges. First, detailed analyses are conducted to investigate the failure and predict the intrinsic nonlinear material properties of a specific aerospace-grade aluminum honeycomb core and carbon-epoxy composite face sheet. Sandwich panels with two types of bonded fittings are chosen to investigate nonlinear effects such as shear buckling and plastic deformation in the honeycomb core, and the progressive damage response in composite skins under different loading conditions. The nonlinear properties and modeling strategies are then incorporated in the subsequent analysis of a spacecraft’s thrust tube sandwich structure subject to cyclic thermal loading. The predicted damage and failure in the thrust tube section with an adhesively bonded cup fitting correlated with experimental observations. The current methodology offers a consistent technique for investigating the thermomechanical performance of sandwich structures with other configurations of bonded joints and fittings. |
| ArticleNumber | 113086 |
| Author | Stoumbos, T. Venkatesan, K.R. Inoyama, D. Chattopadhyay, A. |
| Author_xml | – sequence: 1 givenname: K.R. surname: Venkatesan fullname: Venkatesan, K.R. email: kvenka10@asu.edu organization: School for Engineering of Matter, Transport, and Energy, Arizona State University, Tempe, AZ, United States – sequence: 2 givenname: T. surname: Stoumbos fullname: Stoumbos, T. organization: Space Systems Division, Northrop Grumman Innovation Systems, Dulles, VA, United States – sequence: 3 givenname: D. surname: Inoyama fullname: Inoyama, D. organization: Space Systems Division, Northrop Grumman Innovation Systems, Dulles, VA, United States – sequence: 4 givenname: A. surname: Chattopadhyay fullname: Chattopadhyay, A. organization: School for Engineering of Matter, Transport, and Energy, Arizona State University, Tempe, AZ, United States |
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| CitedBy_id | crossref_primary_10_1016_j_compstruct_2022_116113 crossref_primary_10_1016_j_ijmecsci_2024_109589 crossref_primary_10_1016_j_jobe_2024_111311 crossref_primary_10_1016_j_mechmat_2024_105054 crossref_primary_10_1016_j_ijmecsci_2023_108137 crossref_primary_10_1080_15397734_2022_2104312 crossref_primary_10_3390_s22010153 crossref_primary_10_1016_j_compstruct_2025_118934 crossref_primary_10_1016_j_matpr_2023_08_210 crossref_primary_10_1007_s00161_021_01006_2 crossref_primary_10_1016_j_compstruct_2024_118549 crossref_primary_10_1016_j_geoen_2023_212434 |
| Cites_doi | 10.1016/0020-7403(88)90060-4 10.1016/j.commatsci.2012.01.007 10.2514/6.2010-3100 10.1115/1.1490372 10.1016/j.ijmecsci.2016.04.002 10.1016/j.compstruct.2015.10.044 10.1177/0021998302036007469 10.1023/A:1014344228141 10.1016/j.compstruct.2011.10.018 10.1016/j.compositesb.2012.03.008 10.1016/j.ijsolstr.2004.02.020 10.1115/1.4010217 10.1016/j.compositesa.2007.01.017 10.1016/0167-6636(94)00053-0 10.1016/j.euromechsol.2004.08.004 10.1177/1099636209105378 10.1007/s10704-013-9860-1 10.2514/3.44942 10.1016/j.compscitech.2005.12.023 10.1177/073168448800700205 10.1016/j.msea.2016.03.010 10.1115/1.3225677 10.1016/S0263-8223(97)80013-X 10.1016/j.compstruct.2008.11.013 10.1016/S0263-8223(98)00123-8 10.1177/1099636205046207 10.1016/j.mechmat.2007.03.006 |
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| References | Reddy (b0070) 1984 Hegde, Hojjati (b0005) 2018 Giglio, Gilioli, Manes (b0125) 2012; 56 Matzenmiller, Lubliner, Taylor (b0180) 1995; 20 Yang, Becker (b0105) 2004; 6 Lampman, Zore (b0205) 1990 Lee, Hong, Lee, Kim (b0015) 2002; 37 Liu, Ferreira, Xing, Neves (b0115) 2016; 136 Tuttle (b0010) 2018 Kapuria, Achary (b0085) 2004; 41 Dey, Chattoraj (b0155) 2016; 661 Jirasek (b0175) 2002; 6 Snead, Palazotto (b0030) 1983; 20 Chamis, Aiello, Murthy (b0130) 1986 Pineda, Waas (b0165) 2013; 182 Feldhusen, Warkotsch, Kempf (b0040) 2009; 11 Smith, Banerjee (b0145) 2012; 94 Lapczyk, Hurtado (b0170) 2007; 38 Stoumbos, Setoodeh, Francis, Curtis (b0185) 2014 Ferrari (b0060) 2015 Russell, Liu, Fleck, Deshpande (b0120) 2011; 78 Dafedar, Desai (b0080) 2002; 69 Iarve, Hoos, Braginsky, Zhou, Mollenhauer (b0190) 2015 Frostig, Thomsen (b0095) 2005; 7 Stapleton, Waas, Bednarcyk. Modeling progressive failure of bonded joints using a single joint finite element. NASA/TM—2010-216824; 2010. Li, Wang, Qian, Liu, Qing (b0110) 2016; 111 Heimbs, Pein (b0045) 2009; 89 Chen, Yan (b0160) 2012; 43 Mindlin (b0065) 1951; 18 Shimokawa, Katoh, Hamaguchi, Sanbongi, Mizuno, Nakamura (b0025) 2002; 36 Testing and modeling of Nomex™ honeycomb sandwich Panels with bolt insert. Petras, Sutcliffe (b0055) 1999; 44 Najafizadeh, Heydari (b0075) 2004; 23 Klintworth, Stronge (b0100) 1988; 30 Maimi, Camanho, Mayugo, Davila (b0200) 2007; 39 Park, Kweon, Choi (b0035) 2011 Dattaguru, Everett, Whitcomb, Johnson (b0050) 1984; 106 Sanborn, Morel (b0020) 1988; 7 Frostig (b0090) 1997; 37 Pinho, Robinson, Iannucci (b0195) 2006; 66 Lyford (b0140) 2017 Stoumbos (10.1016/j.compstruct.2020.113086_b0185) 2014 Li (10.1016/j.compstruct.2020.113086_b0110) 2016; 111 Frostig (10.1016/j.compstruct.2020.113086_b0090) 1997; 37 Lampman (10.1016/j.compstruct.2020.113086_b0205) 1990 Petras (10.1016/j.compstruct.2020.113086_b0055) 1999; 44 Chen (10.1016/j.compstruct.2020.113086_b0160) 2012; 43 Klintworth (10.1016/j.compstruct.2020.113086_b0100) 1988; 30 Hegde (10.1016/j.compstruct.2020.113086_b0005) 2018 Dey (10.1016/j.compstruct.2020.113086_b0155) 2016; 661 Feldhusen (10.1016/j.compstruct.2020.113086_b0040) 2009; 11 Lyford (10.1016/j.compstruct.2020.113086_b0140) 2017 Reddy (10.1016/j.compstruct.2020.113086_b0070) 1984 10.1016/j.compstruct.2020.113086_b0150 Kapuria (10.1016/j.compstruct.2020.113086_b0085) 2004; 41 Smith (10.1016/j.compstruct.2020.113086_b0145) 2012; 94 Snead (10.1016/j.compstruct.2020.113086_b0030) 1983; 20 Liu (10.1016/j.compstruct.2020.113086_b0115) 2016; 136 Shimokawa (10.1016/j.compstruct.2020.113086_b0025) 2002; 36 10.1016/j.compstruct.2020.113086_b0135 Lee (10.1016/j.compstruct.2020.113086_b0015) 2002; 37 Tuttle (10.1016/j.compstruct.2020.113086_b0010) 2018 Sanborn (10.1016/j.compstruct.2020.113086_b0020) 1988; 7 Matzenmiller (10.1016/j.compstruct.2020.113086_b0180) 1995; 20 Heimbs (10.1016/j.compstruct.2020.113086_b0045) 2009; 89 Park (10.1016/j.compstruct.2020.113086_b0035) 2011 Ferrari (10.1016/j.compstruct.2020.113086_b0060) 2015 Pinho (10.1016/j.compstruct.2020.113086_b0195) 2006; 66 Maimi (10.1016/j.compstruct.2020.113086_b0200) 2007; 39 Dattaguru (10.1016/j.compstruct.2020.113086_b0050) 1984; 106 Chamis (10.1016/j.compstruct.2020.113086_b0130) 1986 Jirasek (10.1016/j.compstruct.2020.113086_b0175) 2002; 6 Dafedar (10.1016/j.compstruct.2020.113086_b0080) 2002; 69 Yang (10.1016/j.compstruct.2020.113086_b0105) 2004; 6 Giglio (10.1016/j.compstruct.2020.113086_b0125) 2012; 56 Najafizadeh (10.1016/j.compstruct.2020.113086_b0075) 2004; 23 Lapczyk (10.1016/j.compstruct.2020.113086_b0170) 2007; 38 Russell (10.1016/j.compstruct.2020.113086_b0120) 2011; 78 Iarve (10.1016/j.compstruct.2020.113086_b0190) 2015 Frostig (10.1016/j.compstruct.2020.113086_b0095) 2005; 7 Pineda (10.1016/j.compstruct.2020.113086_b0165) 2013; 182 Mindlin (10.1016/j.compstruct.2020.113086_b0065) 1951; 18 |
| References_xml | – volume: 43 start-page: 2107 year: 2012 end-page: 2114 ident: b0160 article-title: Investigation of elastic moduli of Kraft paper honeycomb core sandwich panels publication-title: Compos Part B-Eng – volume: 6 start-page: 319 year: 2004 end-page: 332 ident: b0105 article-title: A comparative investigation of different homogenization methods for prediction of the macroscopic properties of composites publication-title: Comput Model Eng Sci – volume: 56 start-page: 69 year: 2012 end-page: 78 ident: b0125 article-title: Numerical investigation of a three-point bending test on sandwich panels with aluminum skins and Nomex honeycomb core publication-title: Comput Mater Sci – volume: 41 start-page: 4661 year: 2004 end-page: 4684 ident: b0085 article-title: An efficient higher-order zigzag theory for laminated plates subjected to thermal loading publication-title: Int J Solids Struct – year: 2017 ident: b0140 article-title: Failure prediction of honeycomb panel joints using finite element analysis publication-title: Virginia Tech – year: 2015 ident: b0060 article-title: Structurally optimized and additively manufactured inserts for sandwich panels of spacecraft structures – volume: 94 start-page: 820 year: 2012 end-page: 829 ident: b0145 article-title: Reliability of inserts in sandwich composite panels publication-title: Compos Struct – volume: 6 start-page: 1119 year: 2002 end-page: 1132 ident: b0175 article-title: Objective modeling of strain localization publication-title: Rev Fr Genile Civil – year: 2018 ident: b0005 article-title: Thermally induced microcracks and mechanical property of composite honeycomb sandwich structure: experiment and finite element analysis publication-title: J Sandwich Struct Mater – volume: 661 start-page: 168 year: 2016 end-page: 178 ident: b0155 article-title: Interaction of strain rate and hydrogen input on the embrittlement of 7075 T6 Aluminum alloy publication-title: Mater Sci Eng: A – volume: 36 start-page: 885 year: 2002 end-page: 895 ident: b0025 article-title: Effect of thermal cycling on microcracking and strength degradation of high-temperature polymer composite materials for use in next-generation SST structures publication-title: J Compos Mater – volume: 39 start-page: 909 year: 2007 end-page: 919 ident: b0200 article-title: A continuum damage model for composite laminates: Part II – computational implementation and validation publication-title: Mech Mater – volume: 37 start-page: 205 year: 1997 end-page: 221 ident: b0090 article-title: Hygrothermal (environmental) effects in high-order bending of sandwich beams with a flexible core and a discontinuous skin publication-title: Compos Struct – volume: 69 start-page: 790 year: 2002 end-page: 799 ident: b0080 article-title: Thermomechanical buckling of laminated composite plates using mixed, higher-order analytical formulation publication-title: J Appl Mech, Trans ASME – start-page: 592 year: 1990 end-page: 633 ident: b0205 article-title: Properties and selection: nonferrous alloys and special-purpose materials publication-title: ASM Handbook – volume: 44 start-page: 237 year: 1999 end-page: 252 ident: b0055 article-title: Failure mode maps for honeycomb sandwich panels publication-title: Compos Struct – volume: 106 start-page: 59 year: 1984 end-page: 65 ident: b0050 article-title: Geometrically nonlinear analysis of adhesively bonded joints publication-title: J Eng Mater Technol – start-page: 1531 year: 2014 ident: b0185 article-title: Adhesively bonded joint modeling using finite element method for failure mode prediction publication-title: 55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference – volume: 38 start-page: 2333 year: 2007 end-page: 2341 ident: b0170 article-title: Progressive damage modeling in fiber-reinforced materials publication-title: Compos Part A-Appl Sci Manuf – volume: 66 start-page: 2069 year: 2006 end-page: 2079 ident: b0195 article-title: Fracture toughness of the tensile and compressive fibre failure modes in laminated composites publication-title: Compos Sci Technol – volume: 20 start-page: 777 year: 1983 end-page: 783 ident: b0030 article-title: Moisture and temperature effects on the instability of cylindrical composite panels publication-title: J Aircraft – volume: 30 start-page: 273 year: 1988 end-page: 292 ident: b0100 article-title: Elasto-plastic yield limits and deformation laws for transversely crushed honeycombs publication-title: Int J Mech Sci – volume: 89 start-page: 575 year: 2009 end-page: 588 ident: b0045 article-title: Failure behaviour of honeycomb sandwich corner joints and inserts publication-title: Compos Struct – volume: 20 start-page: 125 year: 1995 end-page: 152 ident: b0180 article-title: A constitutive model for anisotropic damage in fiber-composites publication-title: Mech Mater – volume: 136 start-page: 546 year: 2016 end-page: 553 ident: b0115 article-title: Analysis of functionally graded sandwich and laminated shells using a layerwise theory and a differential quadrature finite element method publication-title: Compos Struct – volume: 78 year: 2011 ident: b0120 article-title: Quasistatic three-point bending of carbon fiber sandwich beams with square honeycomb cores publication-title: J Appl Mech, Transctions ASME – reference: Stapleton, Waas, Bednarcyk. Modeling progressive failure of bonded joints using a single joint finite element. NASA/TM—2010-216824; 2010. – year: 1984 ident: b0070 article-title: Energy and variational methods in applied mechanics – volume: 11 start-page: 471 year: 2009 end-page: 486 ident: b0040 article-title: Development of a mechanical technology for joining sandwich elements publication-title: J Sandwich Struct Mater – volume: 37 start-page: 1265 year: 2002 end-page: 1272 ident: b0015 article-title: Mechanical behavior and failure process during compressive and shear deformation of honeycomb composite at elevated temperatures publication-title: J Mater Sci – volume: 23 start-page: 1085 year: 2004 end-page: 1100 ident: b0075 article-title: Thermal buckling of functionally graded circular plates based on higher-order shear deformation plate theory publication-title: Eur J Mech A/Solids – volume: 18 start-page: 31 year: 1951 end-page: 38 ident: b0065 article-title: Influence of transverse shear deformation on the bending of classical plates publication-title: J Appl Mech – volume: 7 start-page: 53 year: 2005 end-page: 75 ident: b0095 article-title: Localized effects in the nonlinear behavior of sandwich panels with a transversely flexible core publication-title: J Sandwich Struct Mater – start-page: 2247 year: 2018 ident: b0010 article-title: Impact of moisture and thermal cycling on delamination fracture toughness of sandwich composites publication-title: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference – volume: 182 start-page: 93 year: 2013 end-page: 122 ident: b0165 article-title: Numerical implementation of a multiple-ISV thermodynamically-based work potential theory for modeling progressive damage and failure in fiber-reinforced laminates publication-title: Int J Fracture – reference: Testing and modeling of Nomex™ honeycomb sandwich Panels with bolt insert. – start-page: 21 year: 2011 end-page: 26 ident: b0035 article-title: Strength of composite sandwich joints under hygrothermal condition publication-title: 18th International Conference on Composites Materials (ICCM) – start-page: 1880 year: 2015 ident: b0190 article-title: Tensile and compression strength prediction in laminated composites by using Discrete Damage Modeling publication-title: 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference – volume: 111 start-page: 101 year: 2016 end-page: 115 ident: b0110 article-title: Static response and free vibration analysis of the composite sandwich structures with multi-layer cores publication-title: Int J Mech Sci – start-page: 370 year: 1986 end-page: 381 ident: b0130 article-title: Fiber composite sandwich thermostructural behavior: computational simulation. Structures publication-title: Proceeding of the Structural Dynamics and Materials Conference – volume: 7 start-page: 155 year: 1988 end-page: 164 ident: b0020 article-title: Effects of thermal cycling on the mechanical and physical properties of a space qualified epoxy adhesive publication-title: J Reinf Plast Compos – volume: 30 start-page: 273 issue: 3–4 year: 1988 ident: 10.1016/j.compstruct.2020.113086_b0100 article-title: Elasto-plastic yield limits and deformation laws for transversely crushed honeycombs publication-title: Int J Mech Sci doi: 10.1016/0020-7403(88)90060-4 – volume: 6 start-page: 319 issue: 4 year: 2004 ident: 10.1016/j.compstruct.2020.113086_b0105 article-title: A comparative investigation of different homogenization methods for prediction of the macroscopic properties of composites publication-title: Comput Model Eng Sci – volume: 56 start-page: 69 year: 2012 ident: 10.1016/j.compstruct.2020.113086_b0125 article-title: Numerical investigation of a three-point bending test on sandwich panels with aluminum skins and Nomex honeycomb core publication-title: Comput Mater Sci doi: 10.1016/j.commatsci.2012.01.007 – ident: 10.1016/j.compstruct.2020.113086_b0150 doi: 10.2514/6.2010-3100 – start-page: 21 year: 2011 ident: 10.1016/j.compstruct.2020.113086_b0035 article-title: Strength of composite sandwich joints under hygrothermal condition – volume: 69 start-page: 790 year: 2002 ident: 10.1016/j.compstruct.2020.113086_b0080 article-title: Thermomechanical buckling of laminated composite plates using mixed, higher-order analytical formulation publication-title: J Appl Mech, Trans ASME doi: 10.1115/1.1490372 – volume: 111 start-page: 101 year: 2016 ident: 10.1016/j.compstruct.2020.113086_b0110 article-title: Static response and free vibration analysis of the composite sandwich structures with multi-layer cores publication-title: Int J Mech Sci doi: 10.1016/j.ijmecsci.2016.04.002 – ident: 10.1016/j.compstruct.2020.113086_b0135 – start-page: 1531 year: 2014 ident: 10.1016/j.compstruct.2020.113086_b0185 article-title: Adhesively bonded joint modeling using finite element method for failure mode prediction – volume: 136 start-page: 546 year: 2016 ident: 10.1016/j.compstruct.2020.113086_b0115 article-title: Analysis of functionally graded sandwich and laminated shells using a layerwise theory and a differential quadrature finite element method publication-title: Compos Struct doi: 10.1016/j.compstruct.2015.10.044 – volume: 78 issue: 3 year: 2011 ident: 10.1016/j.compstruct.2020.113086_b0120 article-title: Quasistatic three-point bending of carbon fiber sandwich beams with square honeycomb cores publication-title: J Appl Mech, Transctions ASME – volume: 6 start-page: 1119 issue: 6 year: 2002 ident: 10.1016/j.compstruct.2020.113086_b0175 article-title: Objective modeling of strain localization publication-title: Rev Fr Genile Civil – volume: 36 start-page: 885 issue: 7 year: 2002 ident: 10.1016/j.compstruct.2020.113086_b0025 article-title: Effect of thermal cycling on microcracking and strength degradation of high-temperature polymer composite materials for use in next-generation SST structures publication-title: J Compos Mater doi: 10.1177/0021998302036007469 – start-page: 1880 year: 2015 ident: 10.1016/j.compstruct.2020.113086_b0190 article-title: Tensile and compression strength prediction in laminated composites by using Discrete Damage Modeling – start-page: 2247 year: 2018 ident: 10.1016/j.compstruct.2020.113086_b0010 article-title: Impact of moisture and thermal cycling on delamination fracture toughness of sandwich composites – volume: 37 start-page: 1265 issue: 6 year: 2002 ident: 10.1016/j.compstruct.2020.113086_b0015 article-title: Mechanical behavior and failure process during compressive and shear deformation of honeycomb composite at elevated temperatures publication-title: J Mater Sci doi: 10.1023/A:1014344228141 – volume: 94 start-page: 820 issue: 3 year: 2012 ident: 10.1016/j.compstruct.2020.113086_b0145 article-title: Reliability of inserts in sandwich composite panels publication-title: Compos Struct doi: 10.1016/j.compstruct.2011.10.018 – year: 1984 ident: 10.1016/j.compstruct.2020.113086_b0070 – start-page: 592 year: 1990 ident: 10.1016/j.compstruct.2020.113086_b0205 article-title: Properties and selection: nonferrous alloys and special-purpose materials – year: 2018 ident: 10.1016/j.compstruct.2020.113086_b0005 article-title: Thermally induced microcracks and mechanical property of composite honeycomb sandwich structure: experiment and finite element analysis publication-title: J Sandwich Struct Mater – year: 2017 ident: 10.1016/j.compstruct.2020.113086_b0140 article-title: Failure prediction of honeycomb panel joints using finite element analysis publication-title: Virginia Tech – volume: 43 start-page: 2107 issue: 5 year: 2012 ident: 10.1016/j.compstruct.2020.113086_b0160 article-title: Investigation of elastic moduli of Kraft paper honeycomb core sandwich panels publication-title: Compos Part B-Eng doi: 10.1016/j.compositesb.2012.03.008 – volume: 41 start-page: 4661 year: 2004 ident: 10.1016/j.compstruct.2020.113086_b0085 article-title: An efficient higher-order zigzag theory for laminated plates subjected to thermal loading publication-title: Int J Solids Struct doi: 10.1016/j.ijsolstr.2004.02.020 – volume: 18 start-page: 31 year: 1951 ident: 10.1016/j.compstruct.2020.113086_b0065 article-title: Influence of transverse shear deformation on the bending of classical plates publication-title: J Appl Mech doi: 10.1115/1.4010217 – volume: 38 start-page: 2333 issue: 11 year: 2007 ident: 10.1016/j.compstruct.2020.113086_b0170 article-title: Progressive damage modeling in fiber-reinforced materials publication-title: Compos Part A-Appl Sci Manuf doi: 10.1016/j.compositesa.2007.01.017 – volume: 20 start-page: 125 issue: 2 year: 1995 ident: 10.1016/j.compstruct.2020.113086_b0180 article-title: A constitutive model for anisotropic damage in fiber-composites publication-title: Mech Mater doi: 10.1016/0167-6636(94)00053-0 – volume: 23 start-page: 1085 year: 2004 ident: 10.1016/j.compstruct.2020.113086_b0075 article-title: Thermal buckling of functionally graded circular plates based on higher-order shear deformation plate theory publication-title: Eur J Mech A/Solids doi: 10.1016/j.euromechsol.2004.08.004 – volume: 11 start-page: 471 issue: 6 year: 2009 ident: 10.1016/j.compstruct.2020.113086_b0040 article-title: Development of a mechanical technology for joining sandwich elements publication-title: J Sandwich Struct Mater doi: 10.1177/1099636209105378 – volume: 182 start-page: 93 issue: 1 year: 2013 ident: 10.1016/j.compstruct.2020.113086_b0165 article-title: Numerical implementation of a multiple-ISV thermodynamically-based work potential theory for modeling progressive damage and failure in fiber-reinforced laminates publication-title: Int J Fracture doi: 10.1007/s10704-013-9860-1 – year: 2015 ident: 10.1016/j.compstruct.2020.113086_b0060 – volume: 20 start-page: 777 issue: 9 year: 1983 ident: 10.1016/j.compstruct.2020.113086_b0030 article-title: Moisture and temperature effects on the instability of cylindrical composite panels publication-title: J Aircraft doi: 10.2514/3.44942 – volume: 66 start-page: 2069 year: 2006 ident: 10.1016/j.compstruct.2020.113086_b0195 article-title: Fracture toughness of the tensile and compressive fibre failure modes in laminated composites publication-title: Compos Sci Technol doi: 10.1016/j.compscitech.2005.12.023 – volume: 7 start-page: 155 issue: 2 year: 1988 ident: 10.1016/j.compstruct.2020.113086_b0020 article-title: Effects of thermal cycling on the mechanical and physical properties of a space qualified epoxy adhesive publication-title: J Reinf Plast Compos doi: 10.1177/073168448800700205 – start-page: 370 year: 1986 ident: 10.1016/j.compstruct.2020.113086_b0130 article-title: Fiber composite sandwich thermostructural behavior: computational simulation. Structures – volume: 661 start-page: 168 year: 2016 ident: 10.1016/j.compstruct.2020.113086_b0155 article-title: Interaction of strain rate and hydrogen input on the embrittlement of 7075 T6 Aluminum alloy publication-title: Mater Sci Eng: A doi: 10.1016/j.msea.2016.03.010 – volume: 106 start-page: 59 issue: 59 year: 1984 ident: 10.1016/j.compstruct.2020.113086_b0050 article-title: Geometrically nonlinear analysis of adhesively bonded joints publication-title: J Eng Mater Technol doi: 10.1115/1.3225677 – volume: 37 start-page: 205 issue: 2 year: 1997 ident: 10.1016/j.compstruct.2020.113086_b0090 article-title: Hygrothermal (environmental) effects in high-order bending of sandwich beams with a flexible core and a discontinuous skin publication-title: Compos Struct doi: 10.1016/S0263-8223(97)80013-X – volume: 89 start-page: 575 issue: 4 year: 2009 ident: 10.1016/j.compstruct.2020.113086_b0045 article-title: Failure behaviour of honeycomb sandwich corner joints and inserts publication-title: Compos Struct doi: 10.1016/j.compstruct.2008.11.013 – volume: 44 start-page: 237 issue: 4 year: 1999 ident: 10.1016/j.compstruct.2020.113086_b0055 article-title: Failure mode maps for honeycomb sandwich panels publication-title: Compos Struct doi: 10.1016/S0263-8223(98)00123-8 – volume: 7 start-page: 53 issue: 1 year: 2005 ident: 10.1016/j.compstruct.2020.113086_b0095 article-title: Localized effects in the nonlinear behavior of sandwich panels with a transversely flexible core publication-title: J Sandwich Struct Mater doi: 10.1177/1099636205046207 – volume: 39 start-page: 909 year: 2007 ident: 10.1016/j.compstruct.2020.113086_b0200 article-title: A continuum damage model for composite laminates: Part II – computational implementation and validation publication-title: Mech Mater doi: 10.1016/j.mechmat.2007.03.006 |
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