Need an answer and explanation to this:
Use your free body diagrams to help you find a solution. Identify the translational (x and z) and rotational (y and z) conditions of equilibrium. Introduce these problems as exemplary applications of the concepts discussed in this part:
An aeroplane of 5 x 104 kg mass is designed with the line of thrust 4 x 10-1 m above the line of drag. In routine flight the drag is 15.2kN, and the centre of pressure on the main plane is 200mm behind the centre of mass. If the centre of pressure on the tailplane is 12m behind the centre of mass, what is the lifting-tail load (FLT)?
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