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Determination of the fatigue crack-growth rate from the fractographic analysis of a specimen representing the aircraft wing skin - MaRDI portal

Determination of the fatigue crack-growth rate from the fractographic analysis of a specimen representing the aircraft wing skin

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Publication:1016313

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DOI10.1016/j.ijfatigue.2008.06.008zbMath1186.74001OpenAlexW1973956102MaRDI QIDQ1016313

Jerzy Kaniowski, Marcin Ciesielski, Włodzimierz Karliński

Publication date: 5 May 2009

Published in: International Journal of Fatigue (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijfatigue.2008.06.008

zbMATH Keywords

aircraft engineering failure analysis fractography crack-growth rate load history reconstruction

Mathematics Subject Classification ID

Brittle fracture (74R10) Experimental work for problems pertaining to mechanics of deformable solids (74-05)

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