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What is RANS Simulation of NACA 23012 Airfoil about?

This thesis investigates the lift coefficient predictions of the NACA 23012 airfoil at low Reynolds numbers through RANS simulations, focusing on the Blade-Vortex Interaction (BVI) relevant to rotorcraft dynamics. The study highlights discrepancies in existing data regarding maximum lift coefficients and angles of attack, necessitating further simulations at high angles of attack for better understanding. Various turbulence models were employed in the simulations, with results aligning with previous RANS st

Author

mokeshdon5.56

Language

EN