A cylindrical 1045 steel bar (Figure 8.34) is subjected to repeated tension- compression stress cycling along its axis. If the load amplitude is \(22,000 \mathrm{~N}\left(4950 \mathrm{lb}_{\mathrm{f}}\right)\), compute the minimum allowable bar diameter to ensure that fatigue failure will not occur. Assume a factor of safety of \(2.0\).

Short Answer

Expert verified
Answer: The minimum allowable diameter for the cylindrical 1045 steel bar is approximately 32.3 mm.

Step by step solution

01

Calculate stress amplitude

First, we need to determine the stress amplitude. This can be calculated using the formula: \(\text{Stress amplitude} = \frac{\text{Load amplitude}}{\text{Area}}\) As we are dealing with a cylindrical bar, the area can be computed using the formula for the area of a circle, which is: \(\text{Area} = \pi \left(\frac{d}{2}\right)^2\) Combining the two formulas, we get: \(\text{Stress amplitude} = \frac{\text{Load amplitude}}{\pi \left(\frac{d}{2}\right)^2}\) We have the load amplitude, which is \(66,700\,N\), and we want to find the minimum allowable diameter (\(d\)) for the cylindrical bar.
02

Determine the allowable stress amplitude using the safety factor

Since we have a safety factor of 2.0, the minimum allowable stress amplitude will be: \(\text{Allowable stress amplitude} = \frac{\text{Stress amplitude}}{\text{Safety factor}}\)
03

Find the minimum diameter

With the equations for Stress amplitude and Allowable stress amplitude, we can now set them equal to each other and solve for the minimum diameter \(d\): \(\frac{\text{Load amplitude}}{\pi \left(\frac{d}{2}\right)^2} = \frac{\text{Stress amplitude}}{\text{Safety factor}}\) To find the diameter, we rearrange the equation as: \(d = 2\sqrt{\frac{\text{Load amplitude} \times \text{Safety factor}}{\pi \times \text{Stress amplitude}}}\) We can plug in the values for load amplitude (\(66,700\,N\)) and the safety factor (2.0). According to the problem, 1045 steel has an endurance limit. We use this value as the stress amplitude, which we can find in the literature or in engineering handbooks. For this example, let's assume that the endurance limit for 1045 steel is 290 MPa or \(290 \times 10^6\, \mathrm{N/m^2}\). \(d = 2\sqrt{\frac{66,700\, \mathrm{N} \times 2.0}{\pi \times 290 \times 10^6\, \mathrm{N/m^2}}}\) Now, we can solve for the minimum diameter \(d\): \(d \approx 0.0323\, \mathrm{m}\) or \(32.3\, \mathrm{mm}\) Therefore, the minimum allowable diameter for the cylindrical 1045 steel bar to ensure that fatigue failure will not occur is approximately \(32.3\, \mathrm{mm}\).

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Cite five factors that may lead to scatter in fatigue life data.

Following is tabulated data that were gathered from a series of Charpy impact tests on a tempered 4140 steel alloy. $$ \begin{array}{rc} \hline \text { Temperature }\left({ }^{\circ} \boldsymbol{C}\right) & \text { Impact Energy }(\boldsymbol{J}) \\ \hline 100 & 89.3 \\ 75 & 88.6 \\ 50 & 87.6 \\ 25 & 85.4 \\ 0 & 82.9 \\ -25 & 78.9 \\ -50 & 73.1 \\ -65 & 66.0 \\ -75 & 59.3 \\ -85 & 47.9 \\ -100 & 34.3 \\ -125 & 29.3 \\ -150 & 27.1 \\ -175 & 25.0 \\ \hline \end{array} $$ (a) Plot the data as impact energy versus temperature. (b) Determine a ductile-to-brittle transition temperature as that temperature corresponding to the average of the maximum and minimum impact energies. (c) Determine a ductile-to-brittle transition temperature as that temperature at which the impact energy is \(70 \mathrm{~J}\).

A cylindrical component constructed from an S-590 alloy (Figure 8.30) has a diameter of 12 \(\mathrm{mm}(0.50\) in.). Determine the maximum load that may be applied for it to survive \(500 \mathrm{~h}\) at \(925^{\circ} \mathrm{C}\left(1700^{\circ} \mathrm{F}\right) .\)

Suppose that a wing component on an aircraft is fabricated from an aluminum alloy that has a plane strain fracture toughness of \(40 \mathrm{MPa} \sqrt{\mathrm{m}}(36.4 \mathrm{ksi} \sqrt{\mathrm{in}}\).). It has been determined that fracture results at a stress of 365 MPa (53,000 psi) when the maximum internal crack length is \(2.5 \mathrm{~mm}(0.10 \mathrm{in} .)\). For this same component and alloy, compute the stress level at which fracture will occur for a critical internal crack length of \(4.0 \mathrm{~mm}(0.16 \mathrm{in}\).).

Briefly explain the difference between fatigue striations and beachmarks in terms of both (a) size and (b) origin.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free