Woodgate, M. A., Barakos, G. N. , Scrase, N. and Neville, T. (2019) Simulation of helicopter ditching using smoothed particle hydrodynamics. Aerospace Science and Technology, 85, pp. 277-292. (doi: 10.1016/j.ast.2018.12.016)
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Abstract
This paper explores the potential use of smoothed particle hydrodynamics methods for helicopter ditching. The method appears suitable for this task since it is mesh-free and can accommodate the interaction between a floating object and the free-surface of water. Simple cases of objects dropped on water were first studied to establish confidence on the method, and quantify the effect of the numerical parameters of SPH including the boundary condition between the water and solid, the effect of the number and type of smoothed particles as well as the generation of different sea-states for the ditching. Once confidence on the method was established, experiments for the ditching of a model-scale helicopter were used for validation. The smoothed particle hydrodynamics method provides good agreement with experiential data for the position and velocity of the helicopter fuselage.
Item Type: | Articles |
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Additional Information: | The financial support via the NGVL project of AgustaWestland and the Business Innovation and Skills Department of UK is gratefully acknowledged. |
Status: | Published |
Refereed: | Yes |
Glasgow Author(s) Enlighten ID: | Barakos, Professor George and Woodgate, Dr Mark |
Authors: | Woodgate, M. A., Barakos, G. N., Scrase, N., and Neville, T. |
College/School: | College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity |
Journal Name: | Aerospace Science and Technology |
Publisher: | Elsevier |
ISSN: | 1270-9638 |
ISSN (Online): | 1626-3219 |
Published Online: | 17 December 2018 |
Copyright Holders: | Copyright © 2018 Elsevier Masson SAS |
First Published: | First published in Aerospace Science and Technology 85: 277-292 |
Publisher Policy: | Reproduced in accordance with the publisher copyright policy |
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