Analytical Assessment of Composite L Angle Strength Under Internal Fuel Pressure in Composite Wing

Autor: KCS, Amardeepa, James, Polagangu, Varughese, Byji

Publikováno v: In Procedia Structural Integrity 2024 60:60-74

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Experimental and numerical investigation of interface damage in composite L-angle sections under four-point bending

Autor: I. Arthur Jones, Xi Zou, M.Y. Matveev, J.P. Rouse, Shibo Yan

Publikováno v: Journal of Composite Materials

Curved laminates in aero-structures, such as the L-angle sections where webs and flanges meet, are prone to delamination due to high interlaminar stresses in these regions. Some efforts to investigate delamination in these structures can be found in

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::94427ec1bb12da58e97163760edeafd3

Experimental and numerical analysis of unfolding failure of L-shaped CFRP specimens

Autor: Léon Ratsifandrihana, Christophe Bouvet, Pierre Journoud, Bruno Castanié, Frédéric Laurin

Publikováno v: Composite Structures
Composite Structures, 2019, 232, 111563, p. 1-13. ⟨10.1016/j.compstruct.2019.111563⟩
Composite Structures, Elsevier, 2019, 232, 111563, p. 1-13. ⟨10.1016/j.compstruct.2019.111563⟩

International audience; Highly curved laminated parts are used at the junction between two different perpendicular panels on aircraft primary structures. Usually, these laminates fail by delamination due to a bending moment, which appears when the pa

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::07e32252997b29dcbe9c7fe123f44dd7
https://hal.science/hal-02382912/document

Experimental investigation of the enhancement of delamination resistance in glass/epoxy curved laminates.

Autor: Dinesh Babu, V.¹ (AUTHOR) dineshbabu1048@gmail.com, Arumugam, V.¹ (AUTHOR), Santulli, C.² (AUTHOR)

Publikováno v: Journal of Materials Science. Oct2023, Vol. 58 Issue 37, p14723-14739. 17p. 4 Color Photographs, 4 Black and White Photographs, 1 Diagram, 3 Charts, 9 Graphs.