Numerical Seakeeping Analysis for a Floating Helicopter After Ditching in WaterSource: Journal of Offshore Mechanics and Arctic Engineering:;2024:;volume( 147 ):;issue: 001::page 11401-1DOI: 10.1115/1.4065709Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This 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.
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contributor author | Katsuno, Eduardo Tadashi | |
contributor author | Peters, Andreas | |
contributor author | el Moctar, Ould | |
date accessioned | 2025-04-21T10:39:16Z | |
date available | 2025-04-21T10:39:16Z | |
date copyright | 7/1/2024 12:00:00 AM | |
date issued | 2024 | |
identifier issn | 0892-7219 | |
identifier other | omae_147_1_011401.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4306629 | |
description abstract | This 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Numerical Seakeeping Analysis for a Floating Helicopter After Ditching in Water | |
type | Journal Paper | |
journal volume | 147 | |
journal issue | 1 | |
journal title | Journal of Offshore Mechanics and Arctic Engineering | |
identifier doi | 10.1115/1.4065709 | |
journal fristpage | 11401-1 | |
journal lastpage | 11401-12 | |
page | 12 | |
tree | Journal of Offshore Mechanics and Arctic Engineering:;2024:;volume( 147 ):;issue: 001 | |
contenttype | Fulltext |