Data for NACA 0012
I need to perform reduced-order modelling of flow over oscillating (only heaving/plunging) NACA 0012 airfoil. I'm also performing simulations in FLUENT to obtain the snapshots for constructing the reduced order model.
However, to validate my simulations I need some benchmark data for NACA 0012 airfoil to compare with. Can anyone please suggest a journal article, conference paper, book, or any authentic literature in which I can find pressure distribution, lift and drag coefficients for NACA 0012 for different heaving amplitudes and frequencies. Preferably, data should be at any constant Re between 100 < Re < 1,000 range.
Appreciate your help,
|All times are GMT -4. The time now is 14:49.|