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Miscellanea Views: 1,121 Downloads: 913 Vol. 10, No. 35 (2016) December 29, 2015 pp. pages 534-550

Static and fatigue experimental tests on a full scale fuselage panel and FEM analyses

Raffaele Sepe, Enrico Armentani, Francesco Caputo

A fatigue test on a full scale panel with complex loading condition and geometry configuration has been carried out using a triaxial test machine. The demonstrator is made up of two skins which are linked by a transversal butt-joint…

10.3221/IGF-ESIS.35.59

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SI: Crack Paths Views: 532 Downloads: 388 Vol. 13, No. 48 (2019) February 26, 2019 pp. 87-96

The crack path in fuselage panel under mixed mode biaxial loading

Alexander Zakharov, Valery Shlyannikov, Andrey Tumanov

This paper provides the background for practical applications of nonlinear fracture resistance parameters for structural integrity assessment of aviation structures with initial cracks. The subject of this numerical study is a fragment of…

10.3221/IGF-ESIS.48.11

Details: The crack path in fuselage panel under mixed mode biaxial loading PDF Visual Abstract

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Miscellanea Views: 884 Downloads: 651 Vol. 5, No. 16 (2011) pp. pages 34-42

Damage tolerance analysis of aircraft reinforced panels

F. Carta, A. Pirondi

This work is aimed at reproducing numerically a campaign of experimental tests performed for the development of reinforced panels, typically found in aircraft fuselage. The bonded reinforcements can significantly reduce the rate of fatigue…

10.3221/IGF-ESIS.16.04

Details: Damage tolerance analysis of aircraft reinforced panels PDF

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Static and fatigue experimental tests on a full scale fuselage panel and FEM analyses

The crack path in fuselage panel under mixed mode biaxial loading

Damage tolerance analysis of aircraft reinforced panels