End-to-end RANS aerodynamics case study of the NASA CRM-HL high-lift wing-body, implemented as a fully scripted PyAnsys/Fluent pipeline (geometry → mesh → solve → post) with an AoA sweep, drag polar, and full project report.
python simulation nasa cfd computational-fluid-dynamics aerodynamics aerospace-engineering ansys-fluent rans pyansys high-lift crm-hl
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Updated
Jun 30, 2026 - Python