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Validation of NACA 0012 against Nasa published;

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Old   November 10, 2015, 11:10
Default Validation of NACA 0012 against Nasa published;
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M Sereez
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Dear Fluent Users;

http://turbmodels.larc.nasa.gov/naca0012_val.html

Referring to this case I have shown link to I am sure every one has worked on it if you are interested in flow in aerospace.

I am having a tough time not knowing how NASA got their Reynolds number as 6 million.

The Reference Temp = 300K or 540 Rankine...
Flow M = 0.15 ~ is roughlu 51.45 m/s
Reference Chord Length = 1m;

Mu or Kinematic viscocity of air at 300k ~= 1.57e-05 m2/s.

And if so: Re = VL/(mu) = Therefore = (51.45 * 1)/(1.57e-05) = 3.28 million.

Can some one express their views

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Shereez
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Old   November 11, 2015, 10:35
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any views?
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Old   November 25, 2017, 11:27
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Did you get an answer in the end?

I changed my kinematic viscosity in FLUENT to reach a Reynolds number of 6million - but I'm not sure if this is correct.
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