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Aerospace 3D textile preform analysis: experimental and mesomodeling

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
For the purpose of predicting how textile preforms affect the quality of the composite material and its performance, the stitched textile preform must be characterized. Experimental compaction analysis and finite element analysis of textile preforms are the main subjects of this paper. The formability parameters of a preform can be changed by the stitching process, according to research on the mechanical properties of preforms conducted during compression testing. The loaddeformation response, which is depicted in detail, had the greatest influence on preform deformation. Less fiber bundle undulation in the plane direction and more stitching thread undulation in the thickness direction were observed during compression of the stitched preform, whereas the stitching thread improved the resistance of the preform to compression loading.
Rocznik
Strony
118--122
Opis fizyczny
Bibliogr. 15 poz., rys., tab.
Twórcy
  • University of Economics, Department of Aerospace Engineering, İzmir, Turkey
  • University of Economics, Department of Aerospace Engineering, İzmir, Turkey
Bibliografia
  • [1] Reinhart J., Overview of Composite Materials, [in:] Handbook of Composites, Springer, 1998.
  • [2] Ivanov D.S., Lomov S., Modelling the structure and behaviour of 2D and 3D woven composites used in aerospace applications, Polymer Composites in the Aerospace Industry, Woodhead Publishing, 2014.
  • [3] Deconinck P., Abdulhamid H., Héreil P., Experimental and numerical study of submillimeter-sized hypervelocity impacts on honeycomb sandwich structures, J. Procedia Engineering 2017, 204, 452-459.
  • [4] Riedel W., Nahme H., White D.M., Clegg R., Hypervelocity impact damage prediction in composites: Part II, experimental investigations and simulations, J. Impact Eng. 2006, 33(1-12), 670-680.
  • [5] NASA Contractor Report, Final Report for Contract NNL13AA11C, 218149, 2104.
  • [6] Tomich A., Clarke S., Integration of Complex Geometry, 3D Woven Preforms via Innovative Stitching Technique, Phase II, Space Technology Mission Directorate, NASA, 2019.
  • [7] Thrash P., Manufacturing of a Stitched Resin Infused Fuselage Test Article, CAMX SAMPE, 2014.
  • [8] Unal P.G., 3D Woven Fabrics, [in:] Woven Fabrics, IntechOpen 2012.
  • [9] Barile C., Casavola C., Pappalettere H., The influence of stitching and unconventional fibres orientation on the tensile properties of CFRP laminates, Compos. Part B Eng. 2017, 110, 248-254.
  • [10] Advani S.G., Murat S., Process Modeling in Composite Manufacturing, CRC Press, 2010.
  • [11] Simacek P., Advani S.G., Resin flow modeling in compliant porous media: An efficient approach for liquid composite molding, International Journal of Material Forming 2018, 11, 503-515.
  • [12] Pierreux G., Van-Hemelrijck D., Massart T., RVE computations for evaluation of microdamage initiation in structural stitched non-crimp fabric composites, Journal of Composite Materials 2020, 30, 4751-4771.
  • [13] Iwata A., Inoue T., Naouar N., Boisse P., Lomov V., Coupled meso-macro simulation of woven fabric local deformation during draping, Composites Part A: Applied Science and Manufacturing 2019, 118, 267-280. tions for evaluation of microdamage initiation in structural stitched non-crimp fabric composites, Journal of Composite Materials 2020, 30, 4751-4771.
  • [14] Huang J., Hamila N., Boisse P., Draping modelization of stitched composite reinforcements, ESAFORM, 26 August 2021.
  • [15] Shen H., Wang P., Legrand X., Liu L., Soulat D., Influence of the tufting pattern on the formability of tufted multilayered preforms, Compos. Struct. 2019, 228, 111356.
Uwagi
Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2024).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-330230c9-212a-42ba-a974-ec10b6a42ef5
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