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18th Aug 2017, 13:51

#1138 (permalink)

Sonbra

Join Date: Jul 2017

Location: Oslo

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Thanks! I do understand the formula. But I don't get the right answer!

The CL is 0.384, the Newton of lift is 588600N (60000X 9.81) the wing area is 105 and the density is 1.225 kg/m3

The answer supposed to be 300knots. But how?

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