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Development of Physics-Based Transition Models for Unstructured-Mesh CFD Codes Using Deep Learning Models
Document ID
20210017604
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Chau-lyan Chang (Langley Research Center Hampton, Virginia, United States)
Date Acquired
June 16, 2021
Subject Category
Acoustics
Meeting Information
Meeting: 2021 AIAA Aviation Forum
Location: Online
Country: US
Start Date: August 2, 2021
End Date: August 6, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.07.09.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Transition Modeling
Transition Prediction
Machine Learning Model
Boundary-Layer Instability

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