How can I set a code for differential equation using George Polya's method
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For a steady banked turn. In such a turn the aircraft uses part of the lift force to provide the centripetal force, the force towards the centre of the turn. Solve the governing differential equation, think ? = ? ?, and demonstrates how it works? I have to use explicit differentiation
Mass 8000 kg
Speed 80 m/s]
Turn radius 250 m
Acceleration due to gravity 9.81 m/s2
I need to calculate forces in x and y direction and then plot a graph of F-t and a position graph but I am not sure where to start please help!!f
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