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August 28, 2014, 08:01
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Force coeffients at 87% blade span
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#1 |
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New Member
Stephen O'Donnell
Join Date: Jun 2014
Location: Ireland
Posts: 7
Rep Power: 12  |
Hi all,
I'm simulating a rotating helicopter rotor with varying pitch in Star-CCM+. I want to measure the lift CL and drag Cd coefficients or even better the normal coefficient Cn at 87% along the blade span. I want to plot these values as they vary with azimuth. Can anyone help? 
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September 2, 2014, 10:51
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#2 |
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Senior Member
Ping
Join Date: Mar 2009
Posts: 556
Rep Power: 20 |
if you explain this with less aero terms then others might understand eg draw an image since i imagine it will be possible using thresholds and reports
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| Tags |
| blade pitch, drag coefficient, lift coefficient, normal coefficient, rotational motion |
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