Implementation and Verification of a Correlation Based Transition Prediction Method
2008 (English)In: 38th Fluid Dynamics Conference and Exhibit, 2008Conference paper (Refereed)
In many applications such as turbine and aircraft design, boundary layer transition prediction is an important topic. This paper deals with the implementation and verification of a correlation based transition prediction method previously presented by Menter and Langtry. The two additional transport equations used for predicting transition and a novel set of equations for the production terms are implemented into the CFD code Edge. The results are compared to the well-known Ercoftac wind tunnel results.
Place, publisher, year, edition, pages
Aircraft design, Boundary layer transitions, CFD codes, Transition prediction methods, Transport equation
IdentifiersURN: urn:nbn:se:kth:diva-9250ScopusID: 2-s2.0-78049490178OAI: oai:DiVA.org:kth-9250DiVA: diva2:37742
38th AIAA Fluid Dynamics Conference and Exhibit; Seattle, WA; United States; 23 June 2008 through 26 June 2008
QC 201009032008-10-132008-10-132014-10-13Bibliographically approved