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Quote:
Originally Posted by The_Russian
Not entirely. I should have clarified my position. For some reason I thought we were speaking directly in reference to winglets. I must have read the first post wrong.
Right, you "misunderstood" You thought the question asked about winglets
Sure, that's why you wrote
Quote:
"Wingtip vorticies help to reduce induced drag by increasing the lateral flow of air over the wing."
Uh-huh, you wrote "wingtip vortices" because you really meant winglets.
Look, it's very clear what you meant, and you clarified exactly what you meant in your second post. Now you are trying to claim you didn't really say that and it's all a big misunderstanding.
I don't like A Squared.
Illini Pilot said:induced drag is related to AOA, not really speed.
I did extensive research on winglets and wingtip vortices at my University. And, it was all done in a sub-sonic wind tunnel. Take that back to basic aerodynamics school.
I got your back Rush.
I can't count how many times I've told a student to pull back on the rudder.
VNugget said:And AOA isn't related to airspeed?
The_Russian said:I did extensive research on winglets and wingtip vortices at my University. And, it was all done in a sub-sonic wind tunnel. Take that back to basic aerodynamics school.
induced drag increase,cathaywannabe said:O.K. smart guys - here is another question.
As an airplane slows and maintains straight and level flight, will induced drag increase or decrease?