Simulation of helicopter ditching using smoothed particle hydrodynamics

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)

[img] Text
174945.pdf - Accepted Version
Restricted to Repository staff only until 17 December 2019.
Available under License Creative Commons Attribution Non-commercial No Derivatives.

23MB

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
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 > Aerospace Sciences
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

University Staff: Request a correction | Enlighten Editors: Update this record