Capturing transition with flow–structure–adaptive KDO RANS model

Author:

Xu Jinglei,Xu Ding,Zhang YangORCID,Bai Junqiang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Transition, Pressure Gradient and Stability Theory;Smith,1956

2. A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region;Van Ingen,1956

3. Automatic transition prediction for three dimensional aircraft configurations using the DLR TAU code;Krumbein,2010

4. Steady and unsteady numerical investigation of transitional shock–boundary-layer-interactions on a fan blade;Becker;Aerosp. Sci. Technol.,2007

5. Active boundary layer control in linear cascades using CFD and artificial neural networks;Svorcan;Aerosp. Sci. Technol.,2014

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