answer ASAP would be appreciated Figure below shows the single degree of freedom control surface/actuator system. The control surface has a moment of inertia J = 576 kg.m² about the hinge, the effectiveactuator stiffness and damping values are k = 10 MN/m and c = 146 kNs/m respectively and the rotation of the control surface is rad. The actuator lever arm has lengtha = 0.5 m. It is assumed that the main surface of the wing is fixed rigidly as shown in the figure. Assume that the system is hit by stone and hence move from rest position by aninitial velocity of v0 = 3 rad/s. Maximum amplitude response is0 (t)000000.89 degrees1.2 degrees1.81 degrees1.45 degrees2.36 degreesсwwwad

Given data in the problem: Moment of inertia of the control surface about the hinge: J = 576 kg.m²…

Figure below shows the single degree of freedom control surface/actuator system. The control surface has a moment of inertia J = actuator stiffness and damping values are k = 10 MN/m and c = 146 kNs/m respectively and the rotation of the control surface is a = 0.5 m. It is assumed that the main surface of the wing is fixed rigidly as shown in the figure. Assume that the system is hit by stone and hence move from rest position by an initial velocity of v0 = 3 rad/s. Maximum amplitude response is 576 kg.m² about the hinge, the effective rad. The actuator lever arm has length

Figure below shows the single degree of freedom control surface/actuator system. The control surface has a moment of inertia J = actuator stiffness and damping values are k = 10 MN/m and c = 146 kNs/m respectively and the rotation of the control surface is a = 0.5 m. It is assumed that the main surface of the wing is fixed rigidly as shown in the figure. Assume that the system is hit by stone and hence move from rest position by an initial velocity of v0 = 3 rad/s. Maximum amplitude response is 576 kg.m² about the hinge, the effective rad. The actuator lever arm has length

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.

Question

answer ASAP would be appreciated

Figure below shows the single degree of freedom control surface/actuator system. The control surface has a moment of inertia J = 576 kg.m² about the hinge, the effective
actuator stiffness and damping values are k = 10 MN/m and c = 146 kNs/m respectively and the rotation of the control surface is rad. The actuator lever arm has length
a = 0.5 m. It is assumed that the main surface of the wing is fixed rigidly as shown in the figure. Assume that the system is hit by stone and hence move from rest position by an
initial velocity of v0 = 3 rad/s. Maximum amplitude response is
0 (t)
00000
0.89 degrees
1.2 degrees
1.81 degrees
1.45 degrees
2.36 degrees
с
www
a
d

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