Abstract
This work deals with the 2D numerical solution of inviscid compressible flow and viscous compressible laminar and turbulent flow around the profile. In a case of turbulent flow algebraic Baldwin-Lomax model is used and compared with Wilcox k-omega model. Calculations are done for NACA 0012 and RAE 2822 airfoil profile for the different angles of upstream flow. Numerical results are compared and discussed with experimental data.
Highlights
IntroductionMathematical models used in this work are based on the solution of the inviscid compressible flow and viscous compressible laminar and turbulent flow around the airfoil
Mathematical models used in this work are based on the solution of the inviscid compressible flow and viscous compressible laminar and turbulent flow around the airfoil.Computational domain represents NACA 0012 and RAE 2822 airfoil profiles
This work deals with the 2D numerical solution of inviscid compressible flow and viscous compressible laminar and turbulent flow around the profile
Summary
Mathematical models used in this work are based on the solution of the inviscid compressible flow and viscous compressible laminar and turbulent flow around the airfoil. Computational domain represents NACA 0012 and RAE 2822 airfoil profiles. The results show differences between the uses of each numerical model and experimental results
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