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.