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    Calculation of g force on an bank of an aeroplane

    can anyone tell me how to calculate G force of an airplane of mass=79015, velocity=257.2 m/s turning uniformly at a radius of 100 meters. I use the formula as f=mv^2/r i don't know if its correct but i get an answer of f=52269876.376 then i substituted in the equation f=ma .. and i got a=...
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