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Along which direction is the lift coefficient |
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April 22, 2012, 16:40 |
Along which direction is the lift coefficient
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#1 |
New Member
Join Date: Feb 2012
Posts: 4
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Hi im doing a 2D CFD case for a NACA foil pitching and heaving. Was just wondering if the lift coefficient given by fluent is normal to the inlet flow or normal to the moving foil at that time instant. Thank you.
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April 22, 2012, 19:32 |
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#2 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,751
Rep Power: 66 |
The user inputs for Drag and Lift coefficient will ask you to input the force vector. The drag and lift coefficients are then calculated with respect to this inputted vector regardless of what the inflow conditions are.
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April 23, 2012, 20:32 |
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#3 |
New Member
Join Date: Feb 2012
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Thank you for replying. So if i input to calculate lift for the foil, it will be normal to the foil and and not respect to the x and y velocities in the global coordinate at that instant. Hope this is what you mean.
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April 23, 2012, 23:29 |
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#4 | |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,751
Rep Power: 66 |
Quote:
It does not care what the global x, y, or local surface normal is. |
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Tags |
cfd, fluent |
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