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2D turbulent flow airfoil simulation - extractingthe values of lift and drag forces and coefficients

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Hi I have performed a series of 2D simulations of an airfoil profile in COMSOL 4.3. The simulations were conducted using the computational model for turbulent flow k-omega. I obtained a set of results in the form of velocity and pressure distributions around the airfoil profile. Now I want to extract the values of lift and drag forces and coefficients. Does anyone know how to do it?

Kind regards Rafał


0 Replies Last Post Jul 12, 2023, 10:09 a.m. EDT
COMSOL Moderator

Hello Rafał Kliza

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