On the extension of RANS/LES methods from incom-pressible to compressible transonic turbulent flows with SBLI

In the present work, a compressible extension of the incompressible RANS and LES models implemented in TermoFluids is carried out. The objective is to solve compressible turbulent flows, i.e. high-Reynolds and high-Mach flows, by means of turbulence modelling. Specifically, transonic turbulent flows where shock-boundary layer interaction (SBLI) is present are the main target due to its practical interest. With this idea in mind, several simulations of the Sajben’s transonic diffuser are presented.

CitationPedro, J., Baez, A., Lehmkuhl, O., Perez, C., Oliva, A. On the extension of RANS/LES methods from incom-pressible to compressible transonic turbulent flows with SBLI. A: International Symposium on Turbulence, Heat and Mass Transfer. "Turbulence, Heat and Mass Transfer 8: proceedings of the Eight International Symposium on Turbulence, Heat and Mass Transfer: Sarajevo, Bosnia and Herzegovina, 15-18 September, 2015". Sarajevo: Begell House, 2015.

URIhttp://hdl.handle.net/2117/103429

ISBN978-1-56700-428-8

Collections

View Usage Statistics

Show full item record

Files	Description	Size	Format	View
E093-ext.pdf		312,9Kb	PDF	Restricted access

All rights reserved. This work is protected by the corresponding intellectual and industrial property rights. Without prejudice to any existing legal exemptions, reproduction, distribution, public communication or transformation of this work are prohibited without permission of the copyright holder

UPCommons. Global access to UPC knowledge

On the extension of RANS/LES methods from incom-pressible to compressible transonic turbulent flows with SBLI

View/Open

Browse