Title: Influence of boundary layer on supersonic cavity flow dynamics
Authors: Togiti, Vamshi
Breuer, Michael  
Longo, José
Language: en_US
Subject (DDC): DDC - Dewey Decimal Classification::000 Informatik, Wissen, Systeme
DDC - Dewey Decimal Classification::500 Naturwissenschaften
DDC - Dewey Decimal Classification::600 Technik
Issue Date: Jun-2009
Publisher: ESA Communication Production Office
Document Type: Conference Object
Source: In: Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles / European Symposium on Aerothermodynamics for Space Vehicles 6 2008 Versailles. - Noordwijk : ESA Communication Production Off., 2009 . - 2009, insges. 7 S.
Journal / Series / Working Paper (HSU): Special publications / European Space Agency 
Volume: 659
Pages: insges. 7 Seiten
Publisher Place: Noordwijk
Conference: European Symposium on Aerothermodynamics for Space Vehicles 6 2008 Versailles 
In the present work, the influence of the on-coming boundary layer on the supersonic cavity flow dynamics is studied using the delayed detached-eddy simulation technique.For this purpose, three different inflow boundary conditions are taken into account, namely a laminar boundary layer, a turbulent boundary layer and finally a turbulent boundary layer with a larger momentum thickness than the previous one. The numerical predictions of these different cases are compared with available experimental data (Zhuang 2007 and Kaufman et al. 1983),which include unsteady pressure spectra, mean velocity and pressure fields, resolved Reynolds stresses, and overall sound pressure level along the cavity floor.
Organization Units (connected with the publication): Strömungsmechanik 
URL: https://api.elsevier.com/content/abstract/scopus_id/66949172786
ISBN: 9789292212230
ISSN: 03796566
Appears in Collections:Publications of the HSU Researchers

Show full item record

CORE Recommender

Google ScholarTM



Items in openHSU are protected by copyright, with all rights reserved, unless otherwise indicated.