Question: how do I find C_L to solve this problem? Determine the Maximum Range (A) for the Gulfstream G550 at 41000 ff. The weight of the

how do I find C_L to solve this problem?

Determine the Maximum Range (A) for the Gulfstream G550 at 41000 ff. The weight of the plane when full of fuel is W'= 97000 lbs, and it holds 6165 gal of fuel (6.67 lhs/gal). The wingspan is 6 = 91.5 ft and the wing platform area is S = 1137 fr. The Oswald efficiency factor is e=@9 and the zero-lift drag coefficient is Cp g = 0.0165. The Thrust Specific Fuel Consumption rate is c, = 0.6414 lb/lb-hr. (Hint: See Example 6.20)

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