KS118.DAT
Here is a wing simulation with this airfoil:
Comparison between NACA and KS118, 2D-simulation
KS118 Cl-alpha polar, including stall region at 1M, comparison with NACA23012 and 23015 included:
Monday, October 26, 2009
KS118
You was able to see the polar of KS118 on the previous blog post. Here is the airfoil in question, it is very similar but slightly different from KS125.
KS118.DAT
Here is a wing simulation with this airfoil:
Comparison between NACA and KS118, 2D-simulation
KS118 Cl-alpha polar, including stall region at 1M, comparison with NACA23012 and 23015 included:
KS118.DAT
Here is a wing simulation with this airfoil:
Comparison between NACA and KS118, 2D-simulation
KS118 Cl-alpha polar, including stall region at 1M, comparison with NACA23012 and 23015 included:
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3 comments:
I was prepared for the drag to be lower in the modern laminar flow section, but I was frankly shocked in seeing how the maximum L/D moved to such wonderfully lower values on your KS sections. You can really fly a plane near the max L/D, where the 21012 section you'd be flying a low L/D at cruise.
Hello Karoliina,
If it's possible to use your profile in Light sport aircraft?
Serg
Hello Karoliina,
If it's possible to use your profile in Light sport aircraft?
Serg
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