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Wall Modelling of an Arfoil.
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2 Geometries
3 Meshes
2 Simulation setups
3 Results
2 Geometries 3 Meshes 2 Simulation setups 3 ResultsAbout this project
To predict the boundary layer distance from the wall by meshing with layer and without layer of an airfoil. Hex domimamt parametric is used for mesh. and adding the region , surface refinements to get the accuarate results. simulation is incompressible , steady state , K-Omega SST Is used. First we run the solution for mesh without layer and postproessing the result Then run the simulation for mesh with layer. compare the results for two simuation . one which is layer gives good result.
