The figure shows a combination of a slender cylindrical fuselage and a small aspect ratio triangular flat
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The figure shows a combination of a slender cylindrical fuselage and a small aspect ratio triangular flat wing with a sweep Angle of 60°, When the fuselage angle of attack is zero and the wing mounting angle is 5°, calculate the lift coefficient of the wing-body assembly with the fuselage cross section area as the characteristic area
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