26Mg
and a
center of mass at G. Initially at take-off the engines provide
a thrust 2T = 5kN
and T′ = 2.5kN . Neglect the mass of the wheels and, due to low velocity,
neglect any lift caused by the wings.
Part A
Determine the magnitude of the
acceleration of the plane.
aG
=
0.288ms2
Part B
Determine the normal reaction on the
nose wheel at A.
NA
=
86.0kN
Part C
Determine the normal reactions on each of the two wing wheels located at
B.
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