Example I The figure shows a turbo-prop aeroplane. The mass of the plane is 7000 kg and its C of G is located the major axisI metre forward of the main under-carriage. The moment of ua of the plane about its C of G,and in the plane of pitching,is 35000 kgm2 a given that the main under-carriage stiffness is 350 kN/m, determine the stiffness of the nose-wheel assembly such that:
i the lowest natural frequency in the vertical plane will be greater the 0.75 Hz {Verify the answer by re-substitution.}
ii the two modes of vibration will be un-coupled {i37.5kN/m;ii87.5 kN/m}
b Given that the nose-wheel assembly stiffness is 37.5 kN/m,and the plane is travelling along the runway at 100 km/hr, determine the minimum wavelength of runway vertical deviation to produce resonance. {22.5m}
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