How can I calculate the center of pressure for a component using CFX Post?
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The expressions for a center of pressure with coordinates (CPX,CPY,CPZ) for a solid with outersurface called wing are: CPX=areaInt(X*Pressure)@wing/areaInt(Pressure)@wing CPY=areaInt(Y*Pressure)@wing/areaInt(Pressure)@wing CPZ=areaInt(Z*Pressure)@wing/areaInt(Pressure)@wing This works well for pressure forces. viscous forces can be added as well. ............ |
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