PPRuNe Forums - View Single Post - I don't agree with this FAA ATPL Question

16th Nov 2015, 13:44

#14 (permalink)

Jetpipe.

Join Date: Mar 2011

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The strength of Wingtip vortex is proportional to the value of Induced drag. Ask your self what is Induced drag and when is it the highest and you 'll understand the question.

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