Laminar flow over airfoil
 

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

If you look into the Micro Air Vehicle Community, there has been a lot of experimental data in Re = 20000 - 80 0000 range.