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...

Full description

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
Tags:	Add Tag No Tags, Be the first to tag this record!