1 / 9

Example 6.1 Tensile Testing of Aluminum Alloy

Example 6.1 Tensile Testing of Aluminum Alloy. Convert the change in length data in Table 6-1 to engineering stress and strain and plot a stress-strain curve. (c)2003 Brooks/Cole, a division of Thomson Learning, Inc. Thomson Learning ™ is a trademark used herein under license.

irmaf
Download Presentation

Example 6.1 Tensile Testing of Aluminum Alloy

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Example 6.1 Tensile Testing of Aluminum Alloy Convert the change in length data in Table 6-1 to engineering stress and strain and plot a stress-strain curve.

  2. (c)2003 Brooks/Cole, a division of Thomson Learning, Inc. Thomson Learning™ is a trademark used herein under license. Figure 6.10 The stress-strain curve for an aluminum alloy from Table 6-1

  3. Example 6.1 SOLUTION

  4. Example 6.3 Young’s Modulus of Aluminum Alloy From the data in Example 6.1, calculate the modulus of elasticity of the aluminum alloy. Use the modulus to determine the length after deformation of a bar of initial length of 50 in. Assume that a level of stress of 30,000 psi is applied. Example 6.3 SOLUTION

  5. Example 6.4 Ductility of an Aluminum Alloy The aluminum alloy in Example 6.1 has a final length after failure of 2.195 in. and a final diameter of 0.398 in. at the fractured surface. Calculate the ductility of this alloy. Example 6.4 SOLUTION

  6. Example 6.5 True Stress and True Strain Calculation Compare engineering stress and strain with true stress and strain for the aluminum alloy in Example 6.1 at (a) the maximum load and (b) fracture. The diameter at maximum load is 0.497 in. and at fracture is 0.398 in. Example 6.5 SOLUTION

  7. Example 6.5 SOLUTION (Continued)

More Related