The effect of emergency floatation system (EFS) on helicopter stability during ditching-Reference-Cited by-同舟云学术

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The effect of emergency floatation system (EFS) on helicopter stability during ditching

Published:2023-12 Issue: Volume:14 Page:100206
ISSN:2666-691X
Container-title:Transportation Engineering
language:en
Short-container-title:Transportation Engineering

Author:

Aziz Adenen,Mad Sariff Elmi Shafik,Shamsudheen Iqbal^ORCID,Abd Jamil Roshamida^ORCID,Abu Zarim Mohamad Abu Ubaidah Amir

Funder

National Defence University of Malaysia

Publisher

Elsevier BV

Subject

Mechanical Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference26 articles.

1. AirSafe.com, Definitions of key terms, http://www.airsafe.com/events/define.htm.

2. Hull slamming;Abrate;Appl. Mech. Rev.,2013

3. Helicopter ditching incident analysis: classification of risk factor;Adenen;J. Eng. Sci. Technol.,2023

4. Simulations of helicopter ditching using smoothed particle hydrodynamics;Oger;J. Hydrodyn.,2020

5. AAIB, Report on the accident to Eurocopter AS332 L2 Super Puma, G-WNSB on approach to Sumburgh Airport in the Shetland Islands, 23 August 2013, 2016. https://www.gov.uk/aaib-reports/aircraft-accident-report-aar-1-2016-g-wnsb-23-august-2013.

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