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23 Nov 2019

A small business jet has a wing area of 21.5 m2 and an aspect ratioof
5. Assume the wing has a NACA 65-210 airfoil, a spanefficiency
factor of 0.9, and a profile drag coefficient of 0.004. Calculatethe
wing lift and drag coefficients if the wing is operating at 6degree
angle-of-attack.

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Nestor Rutherford
Nestor RutherfordLv2
26 Aug 2019

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