An Integral Boundary Layer Method using Discontinuous Galerkin Discretization and Captured Transition Modeling

An Integral Boundary Layer Method using Discontinuous Galerkin Discretization and Captured Transition Modeling

© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. Viscous analysis is crucial for understanding aerodynamic performance metrics such as profile drag. For three-dimensional (3D) viscous analysis, Reynolds-averaged Navier-Stokes (RANS) solvers are often the fas...

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Main Authors: Zhang, Shun-Rong (Author), Drela, Mark (Author), Galbraith, Marshall C. (Author), Allmaras, Steven R. (Author), Darmofal, David L (Author)
Other Authors: Haystack Observatory (Contributor), Massachusetts Institute of Technology. Department of Aeronautics and Astronautics (Contributor)
Format: Article
Language:English
Published: American Institute of Aeronautics and Astronautics (AIAA), 2022-08-23T15:42:15Z.
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