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.
python validation cfd aircraft turbulence fluid-dynamics computational-fluid-dynamics case-study aerodynamics aerospace-engineering boundary-layer panel-method wing-design drag-reduction natural-laminar-flow boundary-layer-transition laminar-turbulent-transition skin-friction-drag transition-modeling
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Updated
Sep 2, 2026 - Python