Large eddy simulation of a complete harrier aircraft in ground effect

This paper aims to demonstrate the viability of using the large eddy simulation (LES) CFD methodology to model a representative, complete STOVL aircraft geometry at touch down. The flowfield beneath such a jet-borne vertical landing aircraft is inherently unsteady. Hence, it is argued in the present...

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Bibliographic Details
Main Authors: Gary Page, Jim McGuirk
Format: Default Article
Published: 2009
Subjects:
Other engineering not elsewhere classified
Science and technology
Technology
Aerospace engineering
Engineering
Engineering not elsewhere classified
Online Access:https://hdl.handle.net/2134/9506
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https://hdl.handle.net/2134/9506

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