Data for NACA 0012

Muntazir · February 5, 2012, 07:09

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

gengatharan · March 28, 2023, 02:59

hi Muntazir sir, have you find any good references for pure plunging experimental data for NACA0012 airfoil?

February 5, 2012, 07:09	Data for NACA 0012	#1
Muntazir New Member Muntazir Naqvi Join Date: Feb 2012 Posts: 4 Rep Power: 14	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

March 28, 2023, 02:59	plunging experimental data for NACA0012 airfoil	#2
gengatharan New Member Gengatharan.R Join Date: Mar 2023 Posts: 2 Rep Power: 0	hi Muntazir sir, have you find any good references for pure plunging experimental data for NACA0012 airfoil?

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