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January 22, 2010, 02:31 |
Calculating forces from wings..
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#1 |
New Member
Join Date: Jan 2010
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Rep Power: 16 |
Please excuse my ignorance but I have a basic question to ask. I've began using CFDesign to start testing some racecar aero properties and want to make sure I'm doing things correctly.
I've got my wing model creating forces in CFDesign, which at 10 deg AoA is around 390 newtons. For planar area, I take the entire area of the wing chord surface and divide by 2, which is 0.528m squared. When I calculate my coefficient of lift I get 0.382 which is 390.027/1215 (dynamic pressure at 45m/s) x 0.528 which is my planform area.. is my calculation correct? Also, is my measurement of the planform area correct, or should I take the exact dimensions of the wing from the top view when its at 10 degrees? Because the wing is angled away, it will be slightly smaller in area from that view.. Thanks for your patience.. |
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January 22, 2010, 23:22 |
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#2 | |
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Skeptic
Join Date: Mar 2009
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Quote:
Sorry to disappoint. |
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January 23, 2010, 15:40 |
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#3 |
New Member
Join Date: Jan 2010
Posts: 4
Rep Power: 16 |
Thanks for your guess.. I assume you came out of the womb with a full understanding of CFD? I see you have nothing better to do on a Friday night so I will just ignore the post. Hopefully someone here is willing to help a beginner. As everyone has to start somewhere
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January 23, 2010, 16:58 |
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#4 |
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Skeptic
Join Date: Mar 2009
Posts: 67
Rep Power: 17 |
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