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January 31, 2014, 02:51 |
Oscillatory cylinder
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Member
alireza
Join Date: Jul 2009
Posts: 32
Rep Power: 15 |
Hi
I try to simulate this paper: A. Rehman, K. Kontis, Synthetic Jet Control Effectiveness on Stationary and Pitching Airfoil. Journal of Aircraft, 2006 in this paper, Dt is 0.0001. When I use this time step flow field is wrong but when I use 0.001 flow field is correct. I don't Know why? Could you help me? I attached these images. 1- steady state before unsteady calculation. 2- unsteady calculation with Dt=0.0001 3- unsteady calculation with Dt=0.001 Excuse me title is oscillatory airfoil, no oscillatory cylinder |
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