Summary At the present time, aerodynamic analysis and numerical methods are inexorably linked. Thus, a quality control system for the aerodynamic simulation of a complete aircraft in varying configurations is very useful. For this purpose it is critical that suitable turbulence models for the various tasks in hand are available to a prospective user. These models should be robust, and yet sufficiently accurate to enable a proper evaluation of the flow in question. This paper provides an overview of the progress in turbulence model implementation in the TAU code during the duration of the MEGAFLOW project.
Turbulence Model Implementation in TAU
2005-01-01
7 pages
Article/Chapter (Book)
Electronic Resource
English
Turbulence Model Implementation in TAU
British Library Conference Proceedings | 2005
|Partially-averaged Navier Stokes Model for Turbulence: Implementation and Validation
British Library Conference Proceedings | 2005
|