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dc.contributor.authorKatsuno, Eduardo Tadashi
dc.contributor.authorPeters, Andreas
dc.contributor.authorel Moctar, Ould
dc.date.accessioned2025-04-21T10:39:16Z
dc.date.available2025-04-21T10:39:16Z
dc.date.copyright7/1/2024 12:00:00 AM
dc.date.issued2024
dc.identifier.issn0892-7219
dc.identifier.otheromae_147_1_011401.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306629
dc.description.abstractThis paper investigates the seakeeping behavior of helicopters after an emergency landing in water, focusing on a Northern North Sea wave climate and considering a realistic helicopter geometry. Computational fluid dynamics techniques, including the cell-centered finite volume method and boundary element methods, were utilized to analyze motion responses and load distribution. The study ensures numerical result reliability through recommended simulation practices. Results indicate that the inviscid model produces similar outcomes to the viscous model in decay tests with roll, pitch, and heave motions. Natural periods for roll, pitch, and heave motions were obtained. Linearity between incident wave amplitude and pitch/heave response was noted for regular waves, while roll linearity was limited for small angles. In irregular wave conditions, helicopters tended to align perpendicular to waves over time, resulting in increased peak roll angles with higher significant wave heights. Exceedance rates of maximum roll peaks, useful for the assessment of capsizing probability, were quantified for different significant wave heights.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleNumerical Seakeeping Analysis for a Floating Helicopter After Ditching in Water
dc.typeJournal Paper
dc.journal.volume147
dc.journal.issue1
dc.journal.titleJournal of Offshore Mechanics and Arctic Engineering
dc.identifier.doi10.1115/1.4065709
dc.journal.fristpage11401-1
dc.journal.lastpage11401-12
dc.page12
dc.treeJournal of Offshore Mechanics and Arctic Engineering:;2024:;volume( 147 ):;issue: 001
dc.contenttypeFulltext


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