not convergence in high angle of attack in low reynold number
why at the angle of attack iof airfoil s increased in the range of 10 degrees, iteration does not converge, but at a low angle of attack 0 to 8 degrees, to achieve convergence, I use the segregated solver, implicit, and K-W turbulence models, why can not achieve convergence. where lies the fault .. I put the inlet velocity boundary conditions of 2.5m / s, and the chord length 1m. help me..
|
Quote:
At high angles of attack, there isn't really a physically meaningful 'steady-state' for you to converge to, the physically meaningful solution is unsteady. |
All times are GMT -4. The time now is 01:12. |