Q4 Figure Q4 shows an aeroplane approaching a runaway for landing. The aeroplane consists of front and rear landing gear set which have different stiffness values. The front landing gear set has stiffness coefficient value, kı = 600 kN/m while the rear landing gear set has stiffness coefficient value, k2 = 700 kN/m. The distance of each landing gear to the center of gravity is l; = 9 m and I2= 2.5 m respectively. The mass of the aeroplane is given as m = 10,000 kg while the radius of gyration, rG= 2 m. By neglecting the damping coefficient of the landing gear: (a) Illustrate the problem as mass-spring system. (b) Construct the equation of motion, complete with all values in the matrix form.

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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Q4 Figure Q4 shows an aeroplane approaching a runaway for landing. The aeroplane consists of
front and rear landing gear set which have different stiffness values. The front landing gear
set has stiffness coefficient value, kı = 600 kN/m while the rear landing gear set has
stiffness coefficient value, k2 = 700 kN/m. The distance of each landing gear to the center
of gravity is l; = 9 m and I2= 2.5 m respectively. The mass of the aeroplane is given as m =
10,000 kg while the radius of gyration, rG= 2 m. By neglecting the damping coefficient of
the landing gear:
(a)
Illustrate the problem as mass-spring system.
(b)
Construct the equation of motion, complete with all values in the matrix form.
Transcribed Image Text:Q4 Figure Q4 shows an aeroplane approaching a runaway for landing. The aeroplane consists of front and rear landing gear set which have different stiffness values. The front landing gear set has stiffness coefficient value, kı = 600 kN/m while the rear landing gear set has stiffness coefficient value, k2 = 700 kN/m. The distance of each landing gear to the center of gravity is l; = 9 m and I2= 2.5 m respectively. The mass of the aeroplane is given as m = 10,000 kg while the radius of gyration, rG= 2 m. By neglecting the damping coefficient of the landing gear: (a) Illustrate the problem as mass-spring system. (b) Construct the equation of motion, complete with all values in the matrix form.
Center of gravity
Rear landing gear set
k2 = 7U0 kN/m
1, = 2.5 m i
Front landing gear set
· I, = 9 m
kj = 6T0 kN/m
Figure Q4
Transcribed Image Text:Center of gravity Rear landing gear set k2 = 7U0 kN/m 1, = 2.5 m i Front landing gear set · I, = 9 m kj = 6T0 kN/m Figure Q4
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