Discrete particle simulation for the initial stages of ice accretion in aircraft engines: initial model development

Buttsworth, David R. and Saleh, Khalid and Yusaf, Talal (2009) Discrete particle simulation for the initial stages of ice accretion in aircraft engines: initial model development. In: 3rd International Conference on Energy and Environment (ICEE 2009): Advancement Towards Global Sustainability, 7-8 Dec 2009, Malacca, Malaysia.

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Abstract

Elements of a discrete particle model that might find application in aircraft engine icing studies are introduced in this paper. As it currently stands, the model is in an embryonic state but it does provides a framework from which further developments can easily proceed. It provides a convenient basis for assessment of aerodynamic particle drag, surface friction, heat transfer and other effects likely to be relevant in the engine icing problem. The model treats the initial stage of accretion, before the inviscid stagnation point flow field is measurably affected by the presence of the ice build-up. The intention is to provide an indication flow field and surface conditions that are likely to lead to stable accretion of ice prior to detectable changes in the aerodynamics of the stagnation point flow field. Preliminary results from the model are presented to demonstrate the current functionality of the model.


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Item Type: Conference or Workshop Item (Commonwealth Reporting Category E) (Paper)
Refereed: Yes
Item Status: Live Archive
Additional Information: Author's version deposited in accordance with the copyright policy of the publisher. '© 2009 IEEE. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE.
Depositing User: Mr Khalid Saleh
Faculty / Department / School: Historic - Faculty of Engineering and Surveying - Department of Mechanical and Mechatronic Engineering
Date Deposited: 05 Jan 2010 01:43
Last Modified: 28 Oct 2014 22:47
Uncontrolled Keywords: aircraft engine icing; ice particle; simulation; aerodynamic particle drag; aircraft engines; discrete particle simulation; embryonic state; engine icing problem; heat transfer; ice accretion; indication flow field; inviscid stagnation point flow field; surface friction
Fields of Research (FOR2008): 09 Engineering > 0913 Mechanical Engineering > 091305 Energy Generation, Conversion and Storage Engineering
08 Information and Computing Sciences > 0801 Artificial Intelligence and Image Processing > 080110 Simulation and Modelling
09 Engineering > 0915 Interdisciplinary Engineering > 091502 Computational Heat Transfer
Socio-Economic Objective (SEO2008): B Economic Development > 88 Transport > 8803 Aerospace Transport > 880303 Air Safety
Identification Number or DOI: 10.1109/ICEENVIRON.2009.5398655
URI: http://eprints.usq.edu.au/id/eprint/6458

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