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The question is long, so I wrote it in the description part, and the you will find the name of the book. (Mechanical Engineering stuff)

I showed that connecting a pressure transducer having a natural frequency of 27,285 Hz (per Example 6.6 in Holman-now you know where the natural frequency of a pressure transducer comes from) to a ramjet combustor wasn’t going to pan out because the combustor has frequencies of 20 KHz, giving us a frequency ratio of 0.733, which, according to Fig 2.6 puts us dangerously close to resonance.  Now that is with an assumed damping ratio of 0.4, which is within reason.

Then I showed you that installing a ‘pigtail’ or a standoff tube would essentially eliminate the problem of ‘ringing,’ thus saving our prescious pressure transducer.  To illustrate that, I pointed you to equation 6.5 to calculate the natural frequency of the pigtail and to equation 6.6 to calculate the damping ratio.

Using the following calculate the natural frequency and damping ratio of the pigtail: tube diameter of 1/4?, tube length of 18?, pressure of two atmospheres, tube air temp of 200 C, and Example 6.2.  Convert to the required units as required and if I didn’t give you a parameter, use Example 6.2.

Calculate the frequency ratio between the pigtail and combustor, refer to Figure 2.6 using the damping ratio you have calculated and verify that you are out of resonance.  Make a copy of the figure and show me where you are by drawing a dot on the figure.

******

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Along the same lines as above, determine the natural freqency of a standard auto tire.  You will need to go the internet or library to find this out.  I prefer for you to find an equation much like 6.5 to describe the natural freqency of the tire.  This is going to be the forcing function frequency of the pressure transducer (the same one as in example 6.6 and use damping ratio of 0.4).  You will prove to yourself that this freqency is well below the natural freqency of the pressure transducer and that you are not ‘ringing’ the transducer.  Draw a dot on a copy of Fig 2.6 showing where you are.

In your research PLEASE CITE YOUR REFERENCES–THIS IS IMPORTANT.

In your research, use search terms such as: cavity resonance, toroid, tire, natural frequency.  You may have to pull a paper or two, in which case this is great opportunity to use the library to help you with this.

Write a two page memo report, double spaced, describing your findings.  Use a standard format of summary, body, conclusion.

******

The Book Name is: Holman Experimental Methods for Engineers 8th edition

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The question is long, so I wrote it in the description part, and the you will find the name of the book. (Mechanical Engineering stuff)

 

 

I showed that connecting a pressure transducer having a natural frequency of 27,285 Hz (per Example 6.6 in Holman-now you know where the natural frequency of a pressure transducer comes from) to a ramjet combustor wasn’t going to pan out because the combustor has frequencies of 20 KHz, giving us a frequency ratio of 0.733, which, according to Fig 2.6 puts us dangerously close to resonance.  Now that is with an assumed damping ratio of 0.4, which is within reason.

Then I showed you that installing a ‘pigtail’ or a standoff tube would essentially eliminate the problem of ‘ringing,’ thus saving our prescious pressure transducer.  To illustrate that, I pointed you to equation 6.5 to calculate the natural frequency of the pigtail and to equation 6.6 to calculate the damping ratio.

Using the following calculate the natural frequency and damping ratio of the pigtail: tube diameter of 1/4″, tube length of 18″, pressure of two atmospheres, tube air temp of 200 C, and Example 6.2.  Convert to the required units as required and if I didn’t give you a parameter, use Example 6.2.

Calculate the frequency ratio between the pigtail and combustor, refer to Figure 2.6 using the damping ratio you have calculated and verify that you are out of resonance.  Make a copy of the figure and show me where you are by drawing a dot on the figure.
******
Along the same lines as above, determine the natural freqency of a standard auto tire.  You will need to go the internet or library to find this out.  I prefer for you to find an equation much like 6.5 to describe the natural freqency of the tire.  This is going to be the forcing function frequency of the pressure transducer (the same one as in example 6.6 and use damping ratio of 0.4).  You will prove to yourself that this freqency is well below the natural freqency of the pressure transducer and that you are not ‘ringing’ the transducer.  Draw a dot on a copy of Fig 2.6 showing where you are.
In your research PLEASE CITE YOUR REFERENCES–THIS IS IMPORTANT.
In your research, use search terms such as: cavity resonance, toroid, tire, natural frequency.  You may have to pull a paper or two, in which case this is great opportunity to use the library to help you with this.
Write a two page memo report, double spaced, describing your findings.  Use a standard format of summary, body, conclusion.
******

 

 

The Book Name is: Holman Experimental Methods for Engineers 8th edition

 

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Stuart L
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Thanks for keeping me sane for getting everything out of the way, I’ve been stuck working more than full time and balancing the rest but I’m glad you’ve been ensuring my school work is taken care of. I'll recommend Elite Academic Research to anyone who seeks quality academic help, thank you so much!
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Brilliant writers and awesome support team. You can tell by the depth of research and the quality of work delivered that the writers care deeply about delivering that perfect grade.
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I really appreciate the work all your amazing writers do to ensure that my papers are always delivered on time and always of the highest quality. I was at a crossroads last semester and I almost dropped out of school because of the many issues that were bombarding but I am glad a friend referred me to you guys. You came up big for me and continue to do so. I just wish I knew about your services earlier.
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You can't fault the paper quality and speed of delivery. I have been using these guys for the past 3 years and I not even once have they ever failed me. They deliver properly researched papers way ahead of time. Each time I think I have had the best their professional writers surprise me with even better quality work. Elite Academic Research is a true Gem among essay writing companies.
Got an A and plagiarism percent was less than 10%! Thanks!

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