Application of a Multimode Transition Model to Turbomachinery Flows
Kozulovic, Dragan (2007) Application of a Multimode Transition Model to Turbomachinery Flows. National Technical University of Athens.
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A transition model is described, which is aimed at turbomachinery flow simulations and can be classified as an integral method based on experimental correlations. This model incorporates all relevant modes of transition and is calibrated on well documented test cases. Besides generic test cases, also multistage turbomachinery configurations are presented, clearly demonstrating the high accuracy of viscous loss predictions. Hence, the presented approach can be used as a tool for the industrial aerodynamic design of highly loaded turbomachinery components.
|Title:||Application of a Multimode Transition Model to Turbomachinery Flows|
|Date:||05 March 2007|
|In ISI Web of Science:||No|
|Number of Pages:||1369|
|Publisher:||National Technical University of Athens|
|Keywords:||transition modelling, turbomachinery flow|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L ER - Engine Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ER - Engine Research|
|DLR - Research theme (Project):||L - Virtual Engine and Validation Methods|
|Institutes and Institutions:||Institute of Propulsion Technology > Numerical Methodes|
|Deposited By:||Dragan Kozulovic|
|Deposited On:||19 Mar 2007|
|Last Modified:||27 Apr 2009 13:36|
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