Implicit large eddy simulation of ship airwakes

dc.contributor.authorThornber, Ben-
dc.contributor.authorStarr, M.-
dc.contributor.authorDrikakis, Dimitris-
dc.date.accessioned2012-03-22T23:01:08Z
dc.date.available2012-03-22T23:01:08Z
dc.date.issued2010-12-31T00:00:00Z-
dc.description.abstractImplicit large eddy simulations (ILES) of two different Royal Navy ships have been conducted as part of the UK Ship/Air Interface Frame-work project using a recently developed very high order accuracy numerical method. Time-accurate CFD data for fourteen flow angles was produced to incorporate into flight simulators for definition of safe helicopter operating limits (SHOLs). This paper discusses the flow phenomenology for the different wind directions and where possible reports on the validation of the ILES results for mean and fluctuating velocity components and spectra against experimental data.en_UK
dc.identifier.citationThornber B, Starr M, Drikakis D., 2010, Implicit large eddy simulation of ship airwakes, Aeronautical Journal, Volume 114, Issue 1162, pp. 715-736
dc.identifier.issn0001-9240-
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7068
dc.language.isoen_UK-
dc.publisherRoyal Aeronautical Societyen_UK
dc.subjecthigh-resolution methods richtmyer-meshkov instability rayleigh-taylor instability reynolds-number flows numerical-simulation compressible flows wing flow turbulence database schemeen_UK
dc.titleImplicit large eddy simulation of ship airwakesen_UK
dc.typeArticle-

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