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...
| Format: | Article |
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| Language: | English |
| Published: |
American Institute of Aeronautics and Astronautics (AIAA),
2021-11-03T16:57:49Z.
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| Subjects: | |
| Online Access: | Get fulltext |