pressure coeffcient of a wing/blade

software: CFD POST ANSYS

menu bar, select Tools > Macro Calculator.

\

correction:

Ref pressure is relative pressure = abs pressure - reference pressure (in Fluent)

definitions;

Cp expression can be defined

as:

(Pressure - $pref [Pa])/dynHead

  • Pressure: static pressure

- $pref the Ref. Pressure set in the macro calculator

- dynHead a reference dynamic head (evaluated at the inlet) that can be defined as:

0.5 * areaAve(Density)@inlet * areaAve(Velocity)@inlet^2

- dynHead is a reference dynamic head



The following information must be specified:

Boundary List: A list of boundaries used in the simulation (blade).

Slice Normal: The axis that will be normal to the slice plane.

Slice Position: The offset of the slice plane in the direction specified by the normal axis.

Inlet Region: The locator used to calculate inlet quantities.

Ref. Pressure: The reference pressure for the simulation.

Plot Axis: The axis on which the results will be plotted.

 

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转载自www.cnblogs.com/code-saturne/p/10809985.html
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