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Please help in solving this aircraft problem.?
An aircraft of 10,000 kg mass is designed with the line of thrust 0.9 meters above the line of drag. In normal flight, the drag is 18.2 kN and the centre of pressure on the main plane is 150 mm behind the C. G. If the centre of pressure of the tail plane is 10 meters behind the C. G. , what is the load on the tail plane in trim condition?
4 Answers
- ?Lv 710 years ago
If you don't understand the question, I'd suggest you talk to your teacher. Asking other people to do your homework for you is cheating.
- Anonymous10 years ago
would be better go to mechanic