The stall angle of attack for the new airfoil is about 14 degrees. With 3 deg of incidence. the nose should not go above 11 deg. Since fuel flow is expected to decrease with additional nose up attitude (less head) just past the expected stall angle seems like a very good place to make sure you have full power capability. Think of the fun on short final if pulling the stick back "just a little bit too far" caused a stall that starved the engine at the same time.
-- wesley scott k...@spottedowl.biz > The other parameter that no one really commented on was the 12.5 deg > nose up attitude. That puts the rudder about 1 1/2 inches off the ground. > Is that a reasonable climb attitude to test at? >
