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22 Jan 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.
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.
Irving HeathcoteLv2
23 Jan 2019