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Muntazir February 5, 2012 07:09

Data for NACA 0012
 
Dear All,

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,


Muntazir


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