An airplane engine and the pylon that attaches it to the wing are idealized as shown below. Drive the equation of motion for small oscillations. Neglect damping and assume free vibration. The rotational spring shown exerts a restoring moment on the pylon (beam ) which is proportional to the angle the pylon makes with the vertical. The engine has a mass moment of inertia la about an axis through its mass center. Assume that the pylon(beam) is rigid and weightless. Solve this problem in terms of: - lo, mass moment of inertia of the engine about its own centroid - W, weight of the engine - K, rotational spring constant - L, length of the pylon
An airplane engine and the pylon that attaches it to the wing are idealized as shown below. Drive the equation of motion for small oscillations. Neglect damping and assume free vibration. The rotational spring shown exerts a restoring moment on the pylon (beam ) which is proportional to the angle the pylon makes with the vertical. The engine has a mass moment of inertia la about an axis through its mass center. Assume that the pylon(beam) is rigid and weightless. Solve this problem in terms of: - lo, mass moment of inertia of the engine about its own centroid - W, weight of the engine - K, rotational spring constant - L, length of the pylon
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Transcribed Image Text:An airplane engine and the pylon that attaches it to the wing are idealized as shown
below. Drive the equation of motion for small oscillations. Neglect damping and assume
free vibration. The rotational spring shown exerts a restoring moment on the pylon
(beam ) which is proportional to the angle the pylon makes with the vertical. The engine
has a mass moment of inertia lo about an axis through its mass center. Assume that the
pylon(beam) is rigid and weightless.
Solve this problem in terms of:
- lo, mass moment of inertia of the engine about its own centroid
- W, weight of the engine
- K, rotational spring constant
- L, length of the pylon
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