Question

PROBLEM I- (3 pts) Figure below represents a suspension system of vehicle. It is composed by a rigid half axle that pivots ab
0 0
Add a comment Improve this question Transcribed image text
Answer #1

1. The equations of motion from Il meelde free Body diogram is Emto - me őt bdor iedo + malsino = Fl free body diagram meo +

Add a comment
Know the answer?
Add Answer to:
PROBLEM I- (3 pts) Figure below represents a suspension system of vehicle. It is composed by...
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for? Ask your own homework help question. Our experts will answer your question WITHIN MINUTES for Free.
Similar Homework Help Questions
  • PLEASE READ CAREFULLY TASK GIVEN BELOW AND ANSWERS THE QUESTIONS WHICH BEEN ASKED A vehicle suspension...

    PLEASE READ CAREFULLY TASK GIVEN BELOW AND ANSWERS THE QUESTIONS WHICH BEEN ASKED A vehicle suspension system can be modelled by the block diagram shown in Figure 1 below: Body mas:s 12 er of s cmicen G, Roac rgut Figure 1: Block diogrom of vehicle suspension system In this block diagram, the variation in the road surface height r as the vehicle moves is the input to the system. The tyre is modelled by the spring and dashpot (damping) system...

  • Problem 1: For the system in figure (1-a), the spring attachment point B is given a horizontal motion Xp-b cos cut from the equilibrium position. The two springs have the same stiffness k 10 N/m and...

    Problem 1: For the system in figure (1-a), the spring attachment point B is given a horizontal motion Xp-b cos cut from the equilibrium position. The two springs have the same stiffness k 10 N/m and the damper has a damping coefficient c. Neglect the friction and mass associated with the pulleys. a) Determine the critical driving frequency for which the oscillations of the mass m tend to become excessively large. b) For a critically damped system, determine damping coefficient...

  • Figure 1 shows a system comprising a bar with mass m=12 kg and the length of...

    Figure 1 shows a system comprising a bar with mass m=12 kg and the length of the bar L=2 m, two springs with stiffness k_t=1000 N-m/rad and k=2000 N/m, one damper with damping coefficient c=50 N-s/m and two additive masses at the end of the bar, where each mass (M) is equal to 50 kg. The rotation about the hinge A, measured with respect to the static equilibrium position of the system is θ(t). The system is excited by force...

  • Problem 3: Find the natural frequency of the system shown in Figure 3. Problem 4: In...

    Problem 3: Find the natural frequency of the system shown in Figure 3. Problem 4: In the mechanical system shown in Figure 4, assume that the rod is massless, perfectly rigid, and pivoted at point P. The displacement x is measured from the equilibrium position. Assuming that x is small, that the weight mg at the end of the rod is 5 N, and that the spring constant k is 400 N/m, find the natural frequency of the system. 2a...

  • i want to get part c,d The figure below is a gear-train mechanical system driven by...

    i want to get part c,d The figure below is a gear-train mechanical system driven by a prescribed motion in the form of an angular displacement y(t). The motion is caused by an applied torque T(t) generated by a motor. The mass moment of inertias of the motor and the driving gear are J and J, respectively, whereas the mass moment of inertias of the load and the driven gear are J, and J2, respectively. The radii and angular displacements...

  • PROBLEMS 89 3-30. A system composed of a mass of S kg and an elastic member having a modulus of 4...

    Please answer 3-34 and 3-35. Please provide all steps so I can follow along. PROBLEMS 89 3-30. A system composed of a mass of S kg and an elastic member having a modulus of 45 N/m is less than critically damped. When the mass is givén an initial displacement and released from rest, the overshoot (the displacement attained past the equilibrium position) is 25% Determine the dam ping factor and the damping constant. 3-31. A mass-spring system is critically damped....

  • Figure Q1 illustrates a simple pressure relief valve system, which consists of a rigid L-shaped beam,...

    Figure Q1 illustrates a simple pressure relief valve system, which consists of a rigid L-shaped beam, hinged at a point where the horizontal part of the beam has length 2L and the vertical part has length L. A spring of stiffness k is attached midway along the horizontal part of the beam, and a damper with damping coefficient c is attached to the vertical part of the beam, at a distance 0.75L from the hinge, O. The pressure relief valve...

  • 3) For the system shown in the figure, the input is the torque T(t) and the...

    3) For the system shown in the figure, the input is the torque T(t) and the outputs are the linear displacements x(t) and the angular displacement θ(t). The equilibrium position corresponds to x 0 0. Note that there is viscous friction between the rack and the surface it slides on. Also, you may treat the small diameter shaft as massless and rigid. mr Clearly state all assumptions to be used for modeling this system. Draw the freebody diagrams. State your...

  • 2. Consider the system shown in the figure below, comprised of the same motor, steel beam,...

    2. Consider the system shown in the figure below, comprised of the same motor, steel beam, steel cable and crate All assumptions and properties are the same with one exception; the cable is no longer considered as rigid Cable properties: length = 4 m, diameter = 0.007 m, E = 207 GPa, Calculate the equivalent stiffness of the cable, in units of N/m. (See table 4.1.1 in your textbook) Draw an equivalent system diagram where the beam and cable each...

  • Problem 4 (25%) Consider the attitude control system of a rigid satellite shown in Figure 1.1....

    Problem 4 (25%) Consider the attitude control system of a rigid satellite shown in Figure 1.1. Fig. 1.1 Satellite tracking control system In this problem we will only consider the control of the angle e (angle of elevation). The dynamic model of the rigid satellite, rotating about an axis perpendicular to the page, can be approximately written as: JÖ = tm - ty - bė where ) is the satellite's moment of inertia, b is the damping coefficient, tm is...

ADVERTISEMENT
Free Homework Help App
Download From Google Play
Scan Your Homework
to Get Instant Free Answers
Need Online Homework Help?
Ask a Question
Get Answers For Free
Most questions answered within 3 hours.
ADVERTISEMENT
ADVERTISEMENT
ADVERTISEMENT