As shown in the figure, there is a long thin wing-body assembly with pointed tips. The body
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As shown in the figure, there is a long thin wing-body assembly with pointed tips. The body of the wing-body connection area is a cylindrical section. Try to find the ratio of cylindrical section R and half span length of the wing l divided by 2l divided by 2 when the ratio of the lift of the assembly 
and the lift of single wing
is minimum in
condition
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