CFD and Machine Learning based aerodynamic drag prediction and optimization using ANSYS Fluent and Python
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Updated
May 28, 2026 - Jupyter Notebook
CFD and Machine Learning based aerodynamic drag prediction and optimization using ANSYS Fluent and Python
Industrial aerodynamics case study predicting laminar-to-turbulent boundary-layer transition over a 3-D natural-laminar-flow aircraft wing (AETHER-NLF 25), using the UTSS multi-mechanism transition solver — includes geometry, mesh, solver outputs, figures, experimental validation, and the full report.
Comparative CFD analysis: NACA 2412 vs NLF airfoils · ~44% L/D improvement at cruise
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