experimental lift and drag coefficients data for the NACA 0012? -- CFD Online Discussion Forums

March 23, 2017, 16:15	experimental lift and drag coefficients data for the NACA 0012?	#1
Seto New Member Join Date: Feb 2017 Posts: 5 Rep Power: 9	I'm looking for experimental lift and drag coefficients data for the NACA 0012 airfoil to validate simulations that I've run. The Reynolds number is 3.00e6. Does anyone have any suggestions regarding where I can find such data?

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