The Chonkerton

Computational Results

science

Per NASA Science, a new page highlights computational results from the fourth and fifth AIAA CFD High Lift Prediction Workshops. The page links to ongoing research on swept‑wing icing and high‑lift aerodynamics. These results are intended to refine design models for future aircraft, supporting next‑generation testing.

Source: https://www.nasa.gov/common_research_model/crm-hl/computa...

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