Schilling, Jakob Christian ; Mittelstedt, Christian (2023)
Approximate postbuckling analysis of shear deformable laminates.
In: PAMM — Proceedings in Applied Mathematics and Mechanics, 23 (4)
doi: 10.1002/pamm.202300082
Artikel, Bibliographie
Dies ist die neueste Version dieses Eintrags.
Kurzbeschreibung (Abstract)
In the lightweight design of aircraft, spacecraft and marine vessels, often advanced materials are utilised. Advanced materials such as laminated composites made of fibre-reinforced plastics show transverse shear deformations if they are considered “thick” or possess little transverse shear stiffness. In most cases, the effect of the shear deformations is neglected, and few computational models exist that consider the closed-form approximate analysis of the postbuckling behaviour. Thus, a new computational model based on high-order shear deformation theories is introduced. The solution is derived based on the principle of the minimum of the total elastic potential and is evaluated in comparison to finite element analyses. The highly efficient approximate computational model is developed to offer a valuable tool for the preliminary design of lightweight structures utilising shear deformable advanced materials.
Typ des Eintrags: | Artikel |
---|---|
Erschienen: | 2023 |
Autor(en): | Schilling, Jakob Christian ; Mittelstedt, Christian |
Art des Eintrags: | Bibliographie |
Titel: | Approximate postbuckling analysis of shear deformable laminates |
Sprache: | Englisch |
Publikationsjahr: | 2023 |
Verlag: | Wiley |
Titel der Zeitschrift, Zeitung oder Schriftenreihe: | PAMM — Proceedings in Applied Mathematics and Mechanics |
Jahrgang/Volume einer Zeitschrift: | 23 |
(Heft-)Nummer: | 4 |
Kollation: | 9 Seiten |
DOI: | 10.1002/pamm.202300082 |
URL / URN: | https://onlinelibrary.wiley.com/doi/10.1002/pamm.202300082 |
Zugehörige Links: | |
Kurzbeschreibung (Abstract): | In the lightweight design of aircraft, spacecraft and marine vessels, often advanced materials are utilised. Advanced materials such as laminated composites made of fibre-reinforced plastics show transverse shear deformations if they are considered “thick” or possess little transverse shear stiffness. In most cases, the effect of the shear deformations is neglected, and few computational models exist that consider the closed-form approximate analysis of the postbuckling behaviour. Thus, a new computational model based on high-order shear deformation theories is introduced. The solution is derived based on the principle of the minimum of the total elastic potential and is evaluated in comparison to finite element analyses. The highly efficient approximate computational model is developed to offer a valuable tool for the preliminary design of lightweight structures utilising shear deformable advanced materials. |
Zusätzliche Informationen: | Special Issue: 93rd Annual Meeting of the International Association of Applied Mathematics and Mechanics (GAMM) |
Fachbereich(e)/-gebiet(e): | 16 Fachbereich Maschinenbau 16 Fachbereich Maschinenbau > Fachgebiet für Konstruktiven Leichtbau und Bauweisen-KLuB (2023 umbenannt in Leichtbau und Strukturmechanik (LSM)) |
Hinterlegungsdatum: | 05 Okt 2023 08:21 |
Letzte Änderung: | 29 Mai 2024 06:22 |
PPN: | 512053413 |
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Verfügbare Versionen dieses Eintrags
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Approximate postbuckling analysis of shear deformable laminates. (deposited 28 Mai 2024 12:09)
- Approximate postbuckling analysis of shear deformable laminates. (deposited 05 Okt 2023 08:21) [Gegenwärtig angezeigt]
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