murtuzaic
New Member
hi guys ,we are building a semi-tapered uav having a tapered section of 700mm and a rectangular section of 470mm ,with a root cord of 400mm and tip chord of 180 mm. we were planning to place our 15 pounds static payload in the wing spar placed at the c.g. of the airfoil.can anyone please help me out with pros and cons of mounting payload in the wing spar.
i was also finding it difficult to calculate the position, size and no. of stringer to be used in the tapered section.i will be oblige if anyone would guide withe the same.
i was also finding it difficult to calculate the position, size and no. of stringer to be used in the tapered section.i will be oblige if anyone would guide withe the same.
