I'm interested in a discussion on the NLF-0215 airfoil on the Lancair 360 and aerodynamic improvements.
Chris Zavatson has added a reflex of up to -7 degrees to gain 10 knots. I hear the wing extensions will increase cruise speed up to 10 knots above 10K feet.
None if these statements is backed by scientific data other than Chris Zavatson reflex study..
I'd like to find an aerodynamics expert to help a lowly mechanical engineer understand the limitations of the 360's airfoil and what can be done to improve it or at least simulate it in Ansys which I have access to as well as Sumulation Hub.