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Cessna 210J Centurion CFD Analysis

This page details the computational fluid dynamics analysis of a Cessna 210J Centurion traveling at 100 KEAS at sea level with a 5-degree angle of attack. Analysis was conducted using STAR CCM+ with a trim mesh of 18.7 million cells and a K-Omega turbulence model. The boundary layer was estimated using Y+ of 100, with 12 prism layers with hyperbolic tangent growth.

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