A Strongly-coupled Non-parametric Integral Boundary Layer Method for Aerodynamic Analysis with Free Transition

A Strongly-coupled Non-parametric Integral Boundary Layer Method for Aerodynamic Analysis with Free Transition

© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. The integral boundary layer (IBL) method with viscous-inviscid coupling is an effective tool for rapid aerodynamic design and analysis. However, existing IBL methods remain to be extended to general three-dime...

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Bibliographic Details
Main Authors: Zhang, Shun, Drela, Mark, Galbraith, Marshall C., Allmaras, Steven R., Darmofal, David L.
Other Authors: Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format: Article
Language:English
Published: American Institute of Aeronautics and Astronautics (AIAA) 2021
Online Access:https://hdl.handle.net/1721.1/137924

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