Automatic Transition Prediction in a Navier–Stokes Solver Using Linear Stability Theory
Author:
Affiliation:
1. Netherlands Aerospace Centre (NLR), 1059 CM Amsterdam, The Netherlands
2. University of Twente, 7522 NB Enschede, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059910
Reference43 articles.
1. LangtryR. B.SenguptaK.YehD. T.DorganA. J. “Extending the γ−Reθt Local Correlation Based Transition Model for Crossflow Effects,” AIAA Paper 2015-2474, 2015. 10.2514/6.2015-2474
2. eN transition prediction for 3D wing configurations using database methods and a local, linear stability code
3. DenisonM.PulliamT. H. “Implementation and Assessment of the Amplification Factor Transport Laminar-Turbulent Transition Model,” AIAA Paper 2018-3382, 2018. 10.2514/6.2018-3382
4. Streamline-Based Transition Prediction Techniques in an Unstructured Computational Fluid Dynamics Code
5. Transition prediction for three-dimensional flows using parallel computation
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