Global stability analysis of a shock wave boundary layer interaction, including a transition model


Abstract eng:
The aim of this is to present a global stability analysis of a shock wave boundary layer interaction which triggers the transition from a laminar to a turbulent state and leads to a separation bubble. The base flow is computed using the k − ω model with the SST correction and the transition model of Langtry. The global stability analysis and the sensitivity analysis take into account not only the laminar and turbulent variables but also the variables leading to the transition process.

Publisher:
International Union of Theoretical and Applied Mechanics, 2016
Conference Title:
Conference Title:
24th International Congress of Theoretical and Applied Mechanics
Conference Venue:
Montreal (CA)
Conference Dates:
2016-08-21 / 2016-08-26
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.



Record appears in:



 Record created 2016-11-15, last modified 2016-11-15


Original version of the author's contribution as presented on CD, page 923, code TS.FM07-2.01 .:
Download fulltext
PDF

Rate this document:

Rate this document:
1
2
3
 
(Not yet reviewed)