A virtual engineering approach to the ship-helicopter dynamic interface – a decade of modelling and simulation research at the University of Liverpool

Author:

Owen I.,White M. D.,Padfield G. D.,Hodge S. J.

Abstract

ABSTRACTThis paper reviews some of the research that has been carried out at the University of Liverpool where the Flight Science and Technology Research Group has developed its Heliflight-R full-motion research simulator to create a simulation environment for the launch and recovery of maritime helicopters to ships. HELIFLIGHT-R has been used to conduct flight trials to produce simulated Ship-Helicopter Operating Limits (SHOLs). This virtual engineering approach has led to a much greater understanding of how the dynamic interface between the ship and the helicopter contributes to the pilot's workload and the aircraft's handling qualities and will inform the conduct of future real-world SHOL trials. The paper also describes how modelling and simulation has been applied to the design of a ship's superstructure to improve the aerodynamic flow field in which the helicopter has to operate. The superstructure aerodynamics also affects the placement of the ship's anemometers and the dispersion of the ship's hot exhaust gases, both of which affect the operational envelope of the helicopter, and both of which can be investigated through simulation.

Publisher

Cambridge University Press (CUP)

Subject

Aerospace Engineering

Reference27 articles.

1. Tai T. and Carico D. Simulation of DD-963 ship airwake by Navier-Stokes method, 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference, 6–9 July 1993, Orlando, Florida, US.

2. Cox I. , Turner G. , Finlay B. and Duncan J. The ship/air interface framework (SAIF) project: Dynamic challenges, Maritime Operations of Rotorcraft, RAeS Conference, 11–12 June 2008, London, UK.

3. Scott P. , Kelly M.F. , White M.D. and Owen I. Using piloted simulation to measure pilot workload of landing a helicopter on a small ship, To be presented at the 43rd European Rotorcraft Forum, 12–15 September 2017, Milan, Italy.

4. Lumsden B. and Padfield G.D. Challenges at the helicopter-ship dynamic interface, Military Aerospace Technologies – Fitec ‘98, IMechE Conference Transactions, 1998, Institution of Mechanical Engineers, Wiley, UK.

5. Forrest J.S. Predicting Ship-Helicopter Operating Limits Using Time-Accurate CFD Ship Airwakes and Piloted Flight Simulation, PhD Thesis, July 2009, University of Liverpool, UK.

Cited by 33 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3