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June 7, 2009, 03:22
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Laminar flow over airfoil
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#1 |
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New Member
Hung
Join Date: May 2009
Posts: 1
Rep Power: 0   |
Dear All!
I am trying to simulate the laminar flow over an airfoil. However, when finding the referent data (Previous researches), it seems no any reference. So I can't understand WHY, maybe that is too old problem or any else reason? Anyone could give me some suggestion about this? Thanks in advance! PAH |
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June 7, 2009, 14:07
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#2 |
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Senior Member
N/A
Join Date: Mar 2009
Posts: 189
Rep Power: 17 |
If you look into the Micro Air Vehicle Community, there has been a lot of experimental data in Re = 20000 - 80 0000 range.
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