The application of a computational method to predict transition for three-dimensional configurations is presented. The method consists of a coupled program system including a 3D Navier-Stokes solver, a transition prediction module, a boundary-layer code and a stability solver. Focus is placed on the industrialization of the method. For this, approaches to treat different, complex three-dimensional aircraft geometries and to account for limitations of the transition prediction method in an industrial computational environment are presented.
Industrialization of the Automatic Transition Prediction in the DLR TAU Code
Notes Numerical Fluid Mech.
2013-01-01
10 pages
Article/Chapter (Book)
Electronic Resource
English
Industrialization of the Automatic Transition Prediction in the DLR TAU Code
British Library Conference Proceedings | 2013
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