@Mig
Always the same, always bragging ... When did I post my "stuff" ? Tell me.
If you gonna be insulting be precise, accurate and honest..
Your Holtzauge did not post detailed calculation or discuss his method. I pointed one source of error. Tht's it.
This is the basis in Sciences. Put it down and submit to what ppl think.
ANd you just hve to open a NACA chart to see the drag rise for the specific airfoil. You don't hve to pick bit of info here and there. It's free and available.
But, huh, tht's what hurt the dark internet genius as always.
And by the way, 10% of drag raise (outsourced from my memory) is equal to what a fully open rad will do on Seversky P-35.
Tht's not negligeable my dear and will certainly not impact the max speed for only 1km/h
Boring...
@Doggle : you are right of course
Last edited by TomcatViP; 10-19-2012 at 04:54 PM.
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