0
Wed Jan 09, 2008 4:49 pm
I would think a big thing is airfoil efficiency. If you look at tables of lift and drag coefficients for a given airfoil profile at varying Reynolds numbers and AoA's, the baseline number is given for an aspect ratio of infinity (ie there are no 'end' effects.. airfoil is infinitely wide). Obviously, this isn't practical to build! The lower the aspect ratio, the less efficient the airfoil will be (cL will be further away from the ideal scenario).
So for a given airfoil plan area, you could have one element with say an aspect ratio of 3.. or you could have 3 airfoils each with an aspect ratio of 9. Higher overall efficiency, more downforce for the least drag.
At least that's my understanding, but I'm not an aerodynamicist by trade..
Grip is a four letter word.
2 is the new #1.