Figure below shows the single degree of freedom control surface/actuator system. The control surface has a moment of inertia J = 30 kg.m² about the hinge, the effective actuator stiffness and damping values are k = 3000 N/m and c = 2640 N.s/m respectively and the rotation of the control surface is rad. The actuator lever arm has length a = 0.2 m. A force f (t) = 108 (t) N is applied to the control surface at a distance d = 1 m from the hinge. It is assumed that the main surface of the wing is fixed rigidly as shown in the figure. Assume small angle approximation. Determine the tip impulse response (displacement at the location of f(t)) at t = 0.082 s 0 (t) f(t) 35.45 mm 11.82 mm 23.64 mm 47.27 mm 7.88 mm

Figure below shows the single degree of freedom control surface/actuator system. The control surface has a moment of inertia J = 30 kg.m² about the hinge, the effective actuator stiffness and damping values are k = 3000 N/m and c = 2640 N.s/m respectively and the rotation of the control surface is rad. The actuator lever arm has length a = 0.2 m. A force f (t) = 108 (t) N is applied to the control surface at a distance d = 1 m from the hinge. It is assumed that the main surface of the wing is fixed rigidly as shown in the figure. Assume small angle approximation. Determine the tip impulse response (displacement at the location of f(t)) at t = 0.082 s 0 (t) f(t) 35.45 mm 11.82 mm 23.64 mm 47.27 mm 7.88 mm

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Concept explainers

Free Damped Vibrations

Free vibration is a type of vibration in which the external force is removed after giving the initial displacement to a body/system. In other words, in this type of vibration, force is applied at the initial displacement of the system, and after the initial displacement, force is removed, and the system vibrates at the natural frequency.

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answer would be greatly appreciated thankyou

Figure below shows the single degree of freedom control surface/actuator system. The control surface has a moment of inertia J = 30 kg.m² about the hinge, the effective
actuator stiffness and damping values are k = 3000 N/m and c = 2640 N.s/m respectively and the rotation of the control surface is rad. The actuator lever arm has
length a = 0.2 m. A force f (t) = 108 (t) N is applied to the control surface at a distance d = 1 m from the hinge. It is assumed that the main surface of the wing is fixed
rigidly as shown in the figure. Assume small angle approximation. Determine the tip impulse response (displacement at the location of f(t)) at t = 0.082 s
0 (t)
f(t)
35.45 mm
11.82 mm
23.64 mm
47.27 mm
7.88 mm
d

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