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Vibration of a cracked cantilever beam full report


Posted by: project report tiger
Created at: Wednesday 17th of February 2010 07:16:54 AM
Last Edited Or Replied at :Wednesday 17th of February 2010 07:16:54 AM
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loading is the formation of a crack that will in the course of time cause the destruction of the structure or the machine part.Vibation is one thing that can never be completely eliminated. Every machine is accompanied by vibration. So the study of response to vibration of such parts with cracks becomes indispensable. The timely intervention to repair the faulty machine part or structure prevents the loss of life as well as money.
3. BASIC CONCEPTS
1. FRACTURE: Fracture is the separation or fragmentation of a solid body into two or more parts under the action of stress. The process of fract..................[:=> Show Contents <=:]



ansys tutorial for leaf spring contact analisys


Posted by:
Created at: Saturday 27th of October 2012 01:18:06 PM
Last Edited Or Replied at :Saturday 27th of October 2012 01:18:06 PM
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I want to know how to make a complete analysis of a fiber reinforced composite leaf spring and a torsional free vibration of a fiber reinforced composi..................[:=> Show Contents <=:]



vibration spectrum analysis book free download


Posted by:
Created at: Thursday 25th of October 2012 12:22:38 PM
Last Edited Or Replied at :Saturday 10th of November 2012 06:55:45 AM
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piezoelectric laminate transducer


Posted by: seminar addict
Created at: Thursday 02nd of February 2012 03:21:27 AM
Last Edited Or Replied at :Thursday 02nd of February 2012 03:21:27 AM
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trical power. Based on Hamilton principle and the assumed mode method, the dyna..................[:=> Show Contents <=:]



UNDAMPED FREE VIBRATION


Posted by: projectsofme
Created at: Saturday 27th of November 2010 12:36:33 AM
Last Edited Or Replied at :Saturday 27th of November 2010 12:36:33 AM
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rential equation of motion by applying Newton’s second law of motion. The third approach to setting up the equation of motion is to apply energy method.
Spring mass system
Fig 2.1 shows a one degree of freedom simple spring mass system. It represents several practical systems. Free vibrations of a system with a single degree of freedom is one of the most important topics. In fig 2.1 the co-ordinate x is used to describe the position of the mass. The mass and spring are the basic building blocks for vibrational analysis. Spring stiffness is defined as the force required to elongate or comp..................[:=> Show Contents <=:]



Microcantilever based force tracking with application to high resolution imaging


Posted by: seminarsense
Created at: Tuesday 16th of November 2010 04:57:16 AM
Last Edited Or Replied at :Tuesday 16th of November 2010 04:57:16 AM
microcantilever beams, microcantilever force resolution ,
ce tracking.
Utilizing MRC PE controller could result in smoother control when compared to commercially avaliable PID controllers.
It significantly enhance the imaging resolution and manipulation accuracy.

References
“nanotechnology”. IEEE Transactions on nanotechnology Vol. 5, No 6, november 2006.
“Microassemblyexperiments under optical vision based control”.IEEE transaction of industrual electronics.Vol 52.No.4,Aug 2005
“Study of data retention of nanocrystal Flash memories”. IEEE International Physics Symposium, April 2003.
“New actuation for push pull electros..................[:=> Show Contents <=:]



Cantilever Beam Sensors


Posted by: rohith.nayanarkn
Created at: Thursday 11th of November 2010 11:21:15 PM
Last Edited Or Replied at :Thursday 11th of November 2010 11:21:15 PM
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C..................[:=> Show Contents <=:]



Vibration of a cracked cantilever beam full report


Posted by: project report tiger
Created at: Wednesday 17th of February 2010 07:16:54 AM
Last Edited Or Replied at :Wednesday 17th of February 2010 07:16:54 AM
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in figure 8 for a/W=0.4 and ß=8.
CRACK AT MID SPAN
With the crack at the mid span, the vibrations of the cantilever beam can be analysed as two spring mass system. With the force ËœF0 sin tâ„¢ , acting at the free end of the beam , the amplitudes ËœY1â„¢ and ËœY2â„¢at the mid span and at the free end, respectively can be written as
(4.15)
and
(4.16)
Where Yst= F0/k1.As a particular case with a/W=0.2, and ß=8, one gets k1/k2=1.276= (1/2)2, and the two natural frequencies are =1.49 1, and =0.6 1.
Figure 9 shows the variation of the amplitudes Y1/Ys..................[:=> Show Contents <=:]



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