no, it is not but the coefficient of 5m is 5×m
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5m=40/5=/5m=8
It is simply: 5m+2
8m + 3n - 5m + 10n = 3m +13n
Assuming -5m=11:Divide both sides by -5: m= -11/5And you have what m equals.
For cylinders coefficient of lift is approximately half of coefficient of drag while they are equal for Aerofoils.