Hi
I am using Sutherland for my aircraft simulation at cruise and would like to know what some parameters mean. I wanted to know whether T0 is total temperature or static temperature at a defined altitude.
Also wanted to know whether V0 is dynamic viscosity at a defined altitude.
Kind regards,
Syed
Hi,
Kindly refer to the following articles:
In short, these values that you see are the Sutherland’s law coefficients for air, and should not be changed.
Cheers
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Hi,
thank for the quick response, just to confirm these values should not be altered even when operating at a altitude + 12,000 m.
Kind regards,
Syed