Docsity
Docsity

Prepare for your exams
Prepare for your exams

Study with the several resources on Docsity


Earn points to download
Earn points to download

Earn points by helping other students or get them with a premium plan


Guidelines and tips
Guidelines and tips

Fundamentals of Vibration: Harmonic Loads and Damping, Study notes of Mechanical Engineering

This lecture from the fundamentals of vibration course covers harmonic loads, resonance, and damping. Topics include the dynamic load magnification factor, the effect of damping on displacement and force transmissibility, and estimating damping from a harmonic load test. Examples and equations are provided.

Typology: Study notes

Pre 2010

Uploaded on 09/17/2009

koofers-user-z4e-1
koofers-user-z4e-1 🇺🇸

10 documents

1 / 14

Toggle sidebar

This page cannot be seen from the preview

Don't miss anything!

bg1
53/58:153 Lecture 9 Fundamental of Vibration
______________________________________________________________________________
- 1 -
Lecture 9: Harmonic Loads (Con’t)
Reading materials: Sections 3.4, 3.5, 3.6 and 3.7
1. Resonance
The dynamic load magnification factor (DLF)
The peak dynamic magnification occurs near r=1 for small damping ratios.
Damping is usually small in practical systems. Therefore, the resonance
condition is usually defined as when the load frequency is same as the undamped
natural frequency.
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe

Partial preview of the text

Download Fundamentals of Vibration: Harmonic Loads and Damping and more Study notes Mechanical Engineering in PDF only on Docsity!


Lecture 9: Harmonic Loads (Con’t)

Reading materials: Sections 3.4, 3.5, 3.6 and 3.

1. Resonance

The dynamic load magnification factor (DLF)

The peak dynamic magnification occurs near r =1 for small damping ratios.

Damping is usually small in practical systems. Therefore, the resonance condition is usually defined as when the load frequency is same as the undamped natural frequency.


Example


Solution is a superposition of sine and cosine harmonic loading

Maximum displacement

Displacement transmissibility: the ratio of maximum displacement with the input displacement a

When the frequency ratio is greater than sqrt(2), the displacement transmitted is less than the static displacement. It means that the damping has a negative effect. In other words, lightly damped systems have lower displacement transmissibility than those with larger damping.


When the frequency ratio is less than sqrt(2), the displacement transmitted is larger than the static displacement. Larger damping values significantly reduce the displacement transmissibility.

Force transmitted to the automobile

Maximum force and force transmissibility


3. Estimating damping from a harmonic load test (Optional)

Dynamic load magnification factor (DLF)

At resonance

Half-power points


Example


Steady state displacement

maximum force

Force transmissibility

When the frequency ratio is greater than sqrt(2), the force transmitted is less than the static force. It is desirable to design foundation so that the frequency ratio at is beyond sqrt(2).

Larger M is better since M increases ω decreases and the frequency ratio increases.

The damping has a negative effect.

Lightly damped systems have lower force transmissibility than those with larger damping.


Example: To design a foundation for a machine that weighs 300 kN. The concrete block supporting the machine is 2.5 x 12 m in plan. Determine its thickness so that only 30% of the static force is transmitted to the supporting structure of this machine. The density of concrete is 1300 kg/m^3. The block is placed on a bed of dry sand and gravel with a coefficient of compression of 0. MPa/m. The damping ratio is 3%. The machine operates at 240 rpm.


6. Stability analysis (Optional)

A system is dynamically stable if the motion (or displacement) converges or remains steady with time.

If the amplitude of displacement increases continuously (diverges) with time, it is said to be dynamically unstable.


7. Self-excitation (Optional)

The force acting on a vibrating system is usually external to the system and independent of the motion.

There are systems for which the exciting force is a function of the motion parameters of the system, such as displacement, velocity, or acceleration.

Such systems are called self-excited vibrating systems since the motion itself produces the exciting force.

The motion diverges and the system becomes unstable if energy is fed into the system through self-excitation.

The instability of rotating shafts, the flutter of turbine blades, the flow-induced vibration of pipes, and the automobile wheel shimmy and aerodynamically induced motion of bridges are typical examples of self-excited vibration.

Example: instability of spring-supported mass on moving belt