Liquid hydrogen storage tank loading generation for civil aircraft damage tolerance analysis

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dc.contributor.authorGiannopoulos, Ioannis K.
dc.contributor.authorTheotokoglou, E. E.
dc.date.accessioned2024-02-15T16:54:20Z
dc.date.available2024-02-15T16:54:20Z
dc.date.issued2023-06-23
dc.description.abstractThe study presented is a preliminary approach and a proposal to the derivation of a loading spectrum for fatigue and damage tolerance analysis for civil aviation Liquid Hydrogen storage tanks. It is anticipated for the first generation of LH2 storage tanks for aviation to utilize metallic lightweight materials. Existing solutions are either too structurally heavy or with a short life span, both constraints making them unsuitable for aircraft vehicles were less mass and longevity is of paramount importance. The objective of the work was to provide suggestions for the generation of representative loading spectra for storage tank fatigue and damage tolerance preliminary design analysis and sizing.en_UK
dc.identifier.citationGiannopoulos IK, Theotokoglou EE. (2023) Liquid hydrogen storage tank loading generation for civil aircraft damage tolerance analysis. In: Journal of Physics: Conference Series, Volume 2692, 7th International Conference of Engineering Against Failure 21-23 June 2023, Spetses Island, Greece. Article number 012048en_UK
dc.identifier.issn1742-6588
dc.identifier.urihttps://doi.org/10.1088/1742-6596/2692/1/012048
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/20817
dc.language.isoenen_UK
dc.publisherAIAAen_UK
dc.rightsAttribution 3.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/3.0/*
dc.titleLiquid hydrogen storage tank loading generation for civil aircraft damage tolerance analysisen_UK
dc.typeConference paperen_UK
dcterms.dateAccepted2022-03-11

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