{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,3,31]],"date-time":"2026-03-31T16:32:20Z","timestamp":1774974740973,"version":"3.50.1"},"reference-count":47,"publisher":"Elsevier BV","license":[{"start":{"date-parts":[[2026,5,1]],"date-time":"2026-05-01T00:00:00Z","timestamp":1777593600000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/www.elsevier.com\/tdm\/userlicense\/1.0\/"},{"start":{"date-parts":[[2026,5,1]],"date-time":"2026-05-01T00:00:00Z","timestamp":1777593600000},"content-version":"tdm","delay-in-days":0,"URL":"https:\/\/www.elsevier.com\/legal\/tdmrep-license"},{"start":{"date-parts":[[2026,2,27]],"date-time":"2026-02-27T00:00:00Z","timestamp":1772150400000},"content-version":"vor","delay-in-days":0,"URL":"http:\/\/creativecommons.org\/licenses\/by-nc-nd\/4.0\/"}],"funder":[{"DOI":"10.13039\/100010663","name":"H2020 European Research Council","doi-asserted-by":"publisher","id":[{"id":"10.13039\/100010663","id-type":"DOI","asserted-by":"publisher"}]},{"DOI":"10.13039\/501100001871","name":"Foundation for Science and Technology","doi-asserted-by":"publisher","id":[{"id":"10.13039\/501100001871","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":["elsevier.com","sciencedirect.com"],"crossmark-restriction":true},"short-container-title":["Thin-Walled Structures"],"published-print":{"date-parts":[[2026,5]]},"DOI":"10.1016\/j.tws.2026.114738","type":"journal-article","created":{"date-parts":[[2026,2,27]],"date-time":"2026-02-27T15:50:52Z","timestamp":1772207452000},"page":"114738","update-policy":"https:\/\/doi.org\/10.1016\/elsevier_cm_policy","source":"Crossref","is-referenced-by-count":0,"special_numbering":"C","title":["Aero-thermo-elastic behaviour of variable stiffness composite laminates and sandwich panels with temperature-dependent material properties"],"prefix":"10.1016","volume":"224","author":[{"ORCID":"https:\/\/orcid.org\/0000-0001-6968-260X","authenticated-orcid":false,"given":"J.A.","family":"Moreira","sequence":"first","affiliation":[]},{"ORCID":"https:\/\/orcid.org\/0000-0001-9287-3519","authenticated-orcid":false,"given":"F.","family":"Moleiro","sequence":"additional","affiliation":[]},{"ORCID":"https:\/\/orcid.org\/0000-0003-3994-2516","authenticated-orcid":false,"given":"A.L.","family":"Ara\u00fajo","sequence":"additional","affiliation":[]},{"ORCID":"https:\/\/orcid.org\/0000-0001-9074-2558","authenticated-orcid":false,"given":"A.","family":"Pagani","sequence":"additional","affiliation":[]}],"member":"78","reference":[{"issue":"1","key":"10.1016\/j.tws.2026.114738_b1","doi-asserted-by":"crossref","first-page":"5","DOI":"10.1002\/msd2.12015","article-title":"Aeroelastic analysis and flutter control of wings and panels: A review","volume":"1","author":"Chai","year":"2021","journal-title":"Int. J. Mech. Syst. Dyn."},{"issue":"9","key":"10.1016\/j.tws.2026.114738_b2","doi-asserted-by":"crossref","first-page":"915","DOI":"10.1080\/01495739.2013.788894","article-title":"About the aerothermoelastic stability of panels in supersonic flows","volume":"36","author":"Baghdasaryan","year":"2013","journal-title":"J. Therm. Stresses"},{"issue":"1","key":"10.1016\/j.tws.2026.114738_b3","doi-asserted-by":"crossref","first-page":"23","DOI":"10.1007\/s12567-013-0054-5","article-title":"Aeroelastic analysis of versatile thermal insulation (VTI) panels with pinched boundary conditions","volume":"6","author":"Carrera","year":"2014","journal-title":"CEAS Space J."},{"key":"10.1016\/j.tws.2026.114738_b4","doi-asserted-by":"crossref","DOI":"10.1016\/j.tws.2024.111885","article-title":"High-frequency vibration analysis of panels under aerothermoelastic effects in supersonic airflow by an energy finite element method","volume":"200","author":"Chen","year":"2024","journal-title":"Thin-Walled Struct."},{"issue":"4","key":"10.1016\/j.tws.2026.114738_b5","doi-asserted-by":"crossref","first-page":"918","DOI":"10.2514\/1.679","article-title":"Linear\/nonlinear supersonic panel flutter in a high-temperature field","volume":"41","author":"Librescu","year":"2004","journal-title":"J. Aircr."},{"issue":"6","key":"10.1016\/j.tws.2026.114738_b6","doi-asserted-by":"crossref","DOI":"10.1061\/(ASCE)AS.1943-5525.0001173","article-title":"Aeroelastic stability and nonlinear flutter analysis of heated panel with temperature-dependent material properties","volume":"33","author":"Ye","year":"2020","journal-title":"J. Aerosp. Eng."},{"issue":"4","key":"10.1016\/j.tws.2026.114738_b7","doi-asserted-by":"crossref","first-page":"360","DOI":"10.2514\/3.7530","article-title":"Supersonic flutter of heated circular cylindrical shells with temperature-dependent material properties","volume":"16","author":"Olsson","year":"1978","journal-title":"AIAA J."},{"issue":"9","key":"10.1016\/j.tws.2026.114738_b8","doi-asserted-by":"crossref","first-page":"4149","DOI":"10.2514\/1.J062976","article-title":"Buckling and fundamental frequency optimization of tow-steered composites using layerwise structural models","volume":"61","author":"Racionero S\u00e1nchez-Majano","year":"2023","journal-title":"AIAA J."},{"key":"10.1016\/j.tws.2026.114738_b9","article-title":"Fundamental frequency layer-wise optimization of tow-steered composites considering gaps and overlaps","author":"Pagani","year":"2024","journal-title":"Aerotec. Missili Spaz."},{"key":"10.1016\/j.tws.2026.114738_b10","doi-asserted-by":"crossref","first-page":"263","DOI":"10.1016\/j.tws.2019.03.040","article-title":"Thermo-mechanical buckling analysis of symmetric VAT composite laminates with temperature-dependent material properties","volume":"140","author":"Li","year":"2019","journal-title":"Thin-Walled Struct."},{"issue":"1","key":"10.1016\/j.tws.2026.114738_b11","doi-asserted-by":"crossref","first-page":"397","DOI":"10.2514\/1.J057282","article-title":"Supersonic flutter and buckling optimization of tow-steered composite plates","volume":"57","author":"Guimar\u00e3es","year":"2019","journal-title":"AIAA J."},{"issue":"1","key":"10.1016\/j.tws.2026.114738_b12","doi-asserted-by":"crossref","first-page":"3","DOI":"10.1007\/s11340-011-9519-7","article-title":"Methodology for obtaining material properties of polymeric foam at elevated temperatures","volume":"52","author":"Zhang","year":"2012","journal-title":"Exp. Mech."},{"key":"10.1016\/j.tws.2026.114738_b13","doi-asserted-by":"crossref","first-page":"91","DOI":"10.1016\/j.compositesb.2016.09.040","article-title":"High-order buckling and free vibration analysis of two types sandwich beam including AL or PVC-foam flexible core and CNTs reinforced nanocomposite face sheets using GDQM","volume":"108","author":"Mohammadimehr","year":"2017","journal-title":"Compos. Part B: Eng."},{"key":"10.1016\/j.tws.2026.114738_b14","series-title":"Finite Element Analysis of Structures Through Unified Formulation","author":"Petrolo","year":"2014"},{"key":"10.1016\/j.tws.2026.114738_b15","doi-asserted-by":"crossref","DOI":"10.1016\/j.compositesb.2019.107388","article-title":"Hygro-thermo-mechanical modelling of multilayered plates: Hybrid composite laminates, fibre metal laminates and sandwich plates","volume":"177","author":"Moleiro","year":"2019","journal-title":"Compos. Part B: Eng."},{"key":"10.1016\/j.tws.2026.114738_b16","doi-asserted-by":"crossref","first-page":"260","DOI":"10.1016\/j.compstruct.2019.02.071","article-title":"Three-dimensional exact hygro-thermo-elastic solutions for multilayered plates: Composite laminates, fibre metal laminates and sandwich plates","volume":"216","author":"Moleiro","year":"2019","journal-title":"Compos. Struct."},{"issue":"4","key":"10.1016\/j.tws.2026.114738_b17","doi-asserted-by":"crossref","DOI":"10.3390\/jcs2040058","article-title":"Thermal buckling behaviour of thin and thick variable-stiffness panels","volume":"2","author":"Vescovini","year":"2018","journal-title":"J. Compos. Sci."},{"key":"10.1016\/j.tws.2026.114738_b18","doi-asserted-by":"crossref","DOI":"10.1016\/j.compstruct.2024.118393","article-title":"Thermal buckling of variable stiffness composite laminates using high order plate finite elements","volume":"345","author":"Bracaglia","year":"2024","journal-title":"Compos. Struct."},{"issue":"4","key":"10.1016\/j.tws.2026.114738_b19","doi-asserted-by":"crossref","first-page":"321","DOI":"10.1080\/01495739.2013.770642","article-title":"Thermo-mechanical buckling analysis of anisotropic multilayered composite and sandwich plates by using refined variable-kinematics theories","volume":"36","author":"Fazzolari","year":"2013","journal-title":"J. Therm. Stresses"},{"issue":"1","key":"10.1016\/j.tws.2026.114738_b20","doi-asserted-by":"crossref","first-page":"1","DOI":"10.1080\/01495739.2012.663679","article-title":"Accurate buckling analysis of composite layered plates with combined thermal and mechanical loadings","volume":"36","author":"Nali","year":"2013","journal-title":"J. Therm. Stresses"},{"issue":"40","key":"10.1016\/j.tws.2026.114738_b21","doi-asserted-by":"crossref","first-page":"5377","DOI":"10.1016\/S0045-7825(01)00172-4","article-title":"Thermal postbuckling behavior of imperfect shear deformable laminated plates with temperature-dependent properties","volume":"190","author":"Shen","year":"2001","journal-title":"Comput. Methods Appl. Mech. Engrg."},{"issue":"4","key":"10.1016\/j.tws.2026.114738_b22","doi-asserted-by":"crossref","first-page":"439","DOI":"10.1016\/j.tws.2007.03.004","article-title":"Thermal buckling analysis of rectangular composite plates with temperature-dependent properties based on a layerwise theory","volume":"45","author":"Shariyat","year":"2007","journal-title":"Thin-Walled Struct."},{"issue":"4","key":"10.1016\/j.tws.2026.114738_b23","doi-asserted-by":"crossref","first-page":"453","DOI":"10.1016\/S0263-8223(01)00117-9","article-title":"Thermal postbuckling analysis of laminated composite plates","volume":"54","author":"Singha","year":"2001","journal-title":"Compos. Struct."},{"issue":"4","key":"10.1016\/j.tws.2026.114738_b24","doi-asserted-by":"crossref","first-page":"1189","DOI":"10.2514\/1.A34378","article-title":"Thermal buckling analysis and optimization of curvilinearly stiffened plates with variable angle tow laminates","volume":"56","author":"Zhao","year":"2019","journal-title":"J. Spacecr. Rockets"},{"key":"10.1016\/j.tws.2026.114738_b25","doi-asserted-by":"crossref","first-page":"313","DOI":"10.1016\/j.compstruct.2018.05.138","article-title":"Aerothermoelastic analysis of composite laminated trapezoidal panels in supersonic airflow","volume":"200","author":"Jiang","year":"2018","journal-title":"Compos. Struct."},{"key":"10.1016\/j.tws.2026.114738_b26","first-page":"887","article-title":"Aerothermoelastic analysis of lattice sandwich composite panels in supersonic airflow","volume":"51","author":"Li","year":"2013","journal-title":"Meccanica"},{"key":"10.1016\/j.tws.2026.114738_b27","doi-asserted-by":"crossref","DOI":"10.1016\/j.tws.2024.112652","article-title":"Isogeometric flutter analysis of a heated laminated plate with and without cutout","volume":"206","author":"Yu","year":"2025","journal-title":"Thin-Walled Struct."},{"key":"10.1016\/j.tws.2026.114738_b28","doi-asserted-by":"crossref","DOI":"10.1016\/j.tws.2020.107180","article-title":"Investigations on nonlinear aerothermoelastic behaviors of multilayered composite panels subject to frictional boundaries and random acoustic loads in supersonic flow","volume":"158","author":"Zhang","year":"2021","journal-title":"Thin-Walled Struct."},{"issue":"23","key":"10.1016\/j.tws.2026.114738_b29","doi-asserted-by":"crossref","first-page":"3253","DOI":"10.1177\/00219983211007542","article-title":"Flutter of variable stiffness composite laminates in supersonic flow with temperature effects","volume":"55","author":"Ouyang","year":"2021","journal-title":"J. Compos. Mater."},{"key":"10.1016\/j.tws.2026.114738_b30","doi-asserted-by":"crossref","first-page":"4327","DOI":"10.1007\/s00707-022-03331-2","article-title":"Aerothermoelastic analysis of curvilinear fiber variable stiffness laminated panels in supersonic flow","volume":"233","author":"Gao","year":"2022","journal-title":"Acta Mech."},{"key":"10.1016\/j.tws.2026.114738_b31","doi-asserted-by":"crossref","first-page":"119","DOI":"10.1016\/j.apm.2024.02.024","article-title":"Aerothermoelastic flutter analysis of variable angle tow composite laminated plates in supersonic flow","volume":"130","author":"Gong","year":"2024","journal-title":"Appl. Math. Model."},{"key":"10.1016\/j.tws.2026.114738_b32","doi-asserted-by":"crossref","DOI":"10.1016\/j.compstruct.2021.114610","article-title":"Nonlinear thermal flutter analysis of variable angle tow composite curved panels in supersonic airflow","volume":"277","author":"Chen","year":"2021","journal-title":"Compos. Struct."},{"issue":"6","key":"10.1016\/j.tws.2026.114738_b33","doi-asserted-by":"crossref","first-page":"835","DOI":"10.1177\/00219983241300147","article-title":"Nonlinear thermal flutter of variable angle tow curved panels with elastically restrained edges in supersonic airflow by generalized Galerkin method","volume":"59","author":"Nie","year":"2025","journal-title":"J. Compos. Mater."},{"key":"10.1016\/j.tws.2026.114738_b34","first-page":"1","article-title":"Variable-kinematic finite elements for the aero-thermo-elastic analysis of variable stiffness composite laminates","author":"Yan","year":"2022","journal-title":"Mech. Adv. Mater. Struct."},{"key":"10.1016\/j.tws.2026.114738_b35","doi-asserted-by":"crossref","DOI":"10.1016\/j.tws.2023.111012","article-title":"Equivalent single layer and layerwise models for flutter and buckling analysis of supersonic variable stiffness laminated composite plates","volume":"191","author":"Moreira","year":"2023","journal-title":"Thin-Walled Struct."},{"key":"10.1016\/j.tws.2026.114738_b36","doi-asserted-by":"crossref","DOI":"10.1016\/j.jsv.2023.118182","article-title":"Layerwise models for supersonic flutter analysis of viscoelastic sandwich panels with curvilinear fibre composite skins","volume":"572","author":"Moreira","year":"2024","journal-title":"J. Sound Vib."},{"key":"10.1016\/j.tws.2026.114738_b37","doi-asserted-by":"crossref","DOI":"10.1016\/j.compstruct.2024.118287","article-title":"Active aeroelastic flutter control of supersonic smart variable stiffness composite panels using layerwise models","volume":"343","author":"Moreira","year":"2024","journal-title":"Compos. Struct."},{"key":"10.1016\/j.tws.2026.114738_b38","doi-asserted-by":"crossref","DOI":"10.1016\/j.ast.2024.109847","article-title":"Active aero-visco-elastic flutter control and layerwise modelling of supersonic smart sandwich panels with variable stiffness composites","volume":"157","author":"Moreira","year":"2025","journal-title":"Aerosp. Sci. Technol."},{"key":"10.1016\/j.tws.2026.114738_b39","doi-asserted-by":"crossref","DOI":"10.1016\/j.compstruct.2025.118920","article-title":"Aero-thermo-elastic stability analysis of supersonic variable stiffness sandwich panels using refined layerwise models","volume":"357","author":"Moreira","year":"2025","journal-title":"Compos. Struct."},{"issue":"7","key":"10.1016\/j.tws.2026.114738_b40","doi-asserted-by":"crossref","first-page":"919","DOI":"10.1007\/s11012-019-00995-4","article-title":"Nonlinear vibrations, bifurcations and chaos of lattice sandwich composite panels on Winkler\u2013pasternak elastic foundations with thermal effects in supersonic airflow","volume":"54","author":"Chai","year":"2019","journal-title":"Meccanica"},{"issue":"4","key":"10.1016\/j.tws.2026.114738_b41","doi-asserted-by":"crossref","first-page":"751","DOI":"10.2514\/3.11613","article-title":"In-plane response of laminates with spatially varying fiber orientations - Variable stiffness concept","volume":"31","author":"G\u00fcrdal","year":"1993","journal-title":"AIAA J."},{"key":"10.1016\/j.tws.2026.114738_b42","doi-asserted-by":"crossref","first-page":"335","DOI":"10.1016\/j.compstruct.2018.03.101","article-title":"Aeroelasticity of composite plates with curvilinear fibres in supersonic flow","volume":"194","author":"Akhavan","year":"2018","journal-title":"Compos. Struct."},{"key":"10.1016\/j.tws.2026.114738_b43","series-title":"Mechanics of Laminated Composite Plates and Shells \u2013 Theory and Analysis","author":"Reddy","year":"2004"},{"key":"10.1016\/j.tws.2026.114738_b44","series-title":"Proceedings of First Symposium on the Theory of Thin Elastic Shells","article-title":"A consistent first approximation in the general theory of thin elastic shells","author":"Koiter","year":"1959"},{"key":"10.1016\/j.tws.2026.114738_b45","doi-asserted-by":"crossref","first-page":"61","DOI":"10.1016\/j.compstruct.2017.07.053","article-title":"Active aerothermoelastic flutter suppression of composite laminated panels with time-dependent boundaries","volume":"179","author":"Chai","year":"2017","journal-title":"Compos. Struct."},{"issue":"8","key":"10.1016\/j.tws.2026.114738_b46","doi-asserted-by":"crossref","first-page":"669","DOI":"10.1080\/01495739.2022.2090471","article-title":"Thermal buckling solutions of generic metallic and laminated structures: Total and updated Lagrangian formulations via refined beam elements","volume":"45","author":"Yan","year":"2022","journal-title":"J. Therm. Stresses"},{"issue":"3","key":"10.1016\/j.tws.2026.114738_b47","doi-asserted-by":"crossref","first-page":"385","DOI":"10.2514\/3.5680","article-title":"Panel flutter - a review of the aeroelastic stability of plates and shells","volume":"8","author":"Dowell","year":"1970","journal-title":"AIAA J."}],"container-title":["Thin-Walled Structures"],"original-title":[],"language":"en","link":[{"URL":"https:\/\/api.elsevier.com\/content\/article\/PII:S0263823126002624?httpAccept=text\/xml","content-type":"text\/xml","content-version":"vor","intended-application":"text-mining"},{"URL":"https:\/\/api.elsevier.com\/content\/article\/PII:S0263823126002624?httpAccept=text\/plain","content-type":"text\/plain","content-version":"vor","intended-application":"text-mining"}],"deposited":{"date-parts":[[2026,3,31]],"date-time":"2026-03-31T14:46:15Z","timestamp":1774968375000},"score":1,"resource":{"primary":{"URL":"https:\/\/linkinghub.elsevier.com\/retrieve\/pii\/S0263823126002624"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2026,5]]},"references-count":47,"alternative-id":["S0263823126002624"],"URL":"https:\/\/doi.org\/10.1016\/j.tws.2026.114738","relation":{},"ISSN":["0263-8231"],"issn-type":[{"value":"0263-8231","type":"print"}],"subject":[],"published":{"date-parts":[[2026,5]]},"assertion":[{"value":"Elsevier","name":"publisher","label":"This article is maintained by"},{"value":"Aero-thermo-elastic behaviour of variable stiffness composite laminates and sandwich panels with temperature-dependent material properties","name":"articletitle","label":"Article Title"},{"value":"Thin-Walled Structures","name":"journaltitle","label":"Journal Title"},{"value":"https:\/\/doi.org\/10.1016\/j.tws.2026.114738","name":"articlelink","label":"CrossRef DOI link to publisher maintained version"},{"value":"article","name":"content_type","label":"Content Type"},{"value":"\u00a9 2026 The Authors. Published by Elsevier Ltd.","name":"copyright","label":"Copyright"}],"article-number":"114738"}}