The load is held in balance by two rods AC and BC, pivotally connected at points A, B and C. The rod of the aircraft is stretched by the force F2 = 45 N, and the rod AC is compressed by the force F1 = 17 N. Determine the weight of the load if angles a = 15 ° and в = 60 °
A detailed solution with a brief description of the condition, formulas and laws used in the solution, the derivation of the formula and the answer.
If you have any questions about the solution, please write. I try to help.
No feedback yet
RU
EN