k-epsilon RNG Drag calculation limitations
1 Attachment(s)
Dear colleagues,
I am working on my masters thesis and i have done a static validation of a NACA 0024 airfoil. I used the k-epsilon RNG model. I have done a calculation of the lift and drag coefficients at different angels of attack, for the drag coefficient i found that my values follow the same curve as the real ones but are way higher. Is there an explenation for this? I added an image of the problem. I need find one to explain this in my thesis preferable with a reference to some klind of paper but i can't find an explanation. Thank you! |
All times are GMT -4. The time now is 00:07. |