Cfd & fluent (k-e turb.model and mesh)

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SUMMARY

This discussion focuses on generating a mesh for an airfoil using ANSYS FLUENT with the k-epsilon turbulent model. The key requirement is to maintain a Y+ value of the first cell within the range of 30-300 for effective wall function application. The conversation highlights the process of creating a Cartesian grid and applying complex transformations to wrap it around the airfoil, which optimizes the mesh for accurate simulations. Additionally, the use of a Joukowski airfoil is recommended for testing due to its analytically generated shape, allowing for validation against known solutions.

PREREQUISITES
  • Understanding of ANSYS FLUENT and its mesh generation capabilities
  • Familiarity with the k-epsilon turbulent model
  • Knowledge of Y+ values and their significance in CFD simulations
  • Experience with grid generation techniques, specifically Sheared Parabolic Grid Generation
NEXT STEPS
  • Research the process of Sheared Parabolic Grid Generation for CFD applications
  • Learn how to calculate Y+ values for mesh refinement near walls
  • Explore the properties and applications of Joukowski airfoils in fluid dynamics
  • Study advanced mesh generation techniques in ANSYS FLUENT for complex geometries
USEFUL FOR

CFD engineers, aerodynamicists, and researchers involved in fluid dynamics simulations, particularly those working with airfoil designs and mesh optimization in ANSYS FLUENT.

mech5190
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Hi. I want to make a mesh for a airfoil for i solute it with FLUENT.
I must use the k-e turbulent model but i do not know how i make the mesh near the wall of airfoil. I have read that the Y plus of first cell must be within 30-300 for standard wall function.
However, How can i compute the Y length of cells for i make the mesh arround the foil?
Is there a specific prosses for the constraction of mesh?
 
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Do a search for "Sheared Parabolic Grid Generation". This is a common analytic grid generation technique. In fact...I think I've posted the method on here some while back.

The idea is that you create a cartesian grid, then "wrap" it around the airfoil using complex transforms. This will give you the best possible grid for solving an airfoil.

Might I also suggest using a "Joukowski" Airfoil to test with. This is an analytically generated airfoil shape (once again using complex transforms). Because it's an analytic shape, analytic solutions exist that you can validate against.
 

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