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This study presents a computational fluid dynamics (CFD) analysis of the NACA 23024 airfoil at a Reynolds number of 6 million, utilizing various turbulence models to assess flow separation. The results from the CFD analysis were compared with wind tunnel data, demonstrating good agreement and providing insights into the performance of different turbulence models. The research emphasizes the advantages of CFD over traditional experimental methods in aerodynamic design and analysis.

Author

Gangchill Unish

Language

EN