Hello all,
Where can I find post stall airfoil data? I'm writing a numerical methods program and need lift coefficient data for airfoils at very high angles of attack. Books or websites would be great.
Thank you for any help
Think you very much for your help. Eliminating the relativa radial positions of the blade that ranged from 0 to 0.1 makes sense. Your explanation on the tangential and axial components of the resultant flow also was of great help as it helped me understand the expected results. I'll keep you...
Hello all,
I have been attempting to perform the iterative procedure outlined in McCormic's textbook (1995) for the vortex theory of propellers. However, I have become stumped when attempting to get tangential velocity relative to tip speed after the first iteration as a part of the equation is...