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  • FLUENT - Flow over an Airfoil- Step 6

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Pressure Coefficient is a dimensionless parameter defined by the equation

Latex

\large
$$
{C_p} = {{(p-p_{ref})} \over q_{ref}}
$$

where p is the static pressure,
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qref is the reference dynamic pressure defined by

\large
$$
q_{ref} = {1 \over 2}\rho_{ref}{v_{ref}}^2
$$

 Latex
The reference pressure, density, and velocity are defined in the Reference Values panel in Step 5. Please refer to FLUENT's help for more information. Go to Help > User's Guide Index for help.
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