|February 5, 2012, 07:09||
Data for NACA 0012
Join Date: Feb 2012
Posts: 4Rep Power: 6
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,
|heave, naca 0012, oscillating, plunge|
|Thread||Thread Starter||Forum||Replies||Last Post|
|3D NACA 0012 Hydrofoil analysis data||sayeem||Main CFD Forum||3||October 16, 2011 11:53|
|NACA 0012 Experimental Data||prasad84||Main CFD Forum||3||July 20, 2011 12:45|
|NACA 0012 data||pixie||Main CFD Forum||3||August 5, 2009 03:01|
|How to update polyPatchbs localPoints||liu||OpenFOAM Running, Solving & CFD||6||December 30, 2005 18:27|
|NACA 0012 data for Low Re||Khurram||Main CFD Forum||5||May 10, 2005 11:05|