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The results shown below were obtained from a tensile test on a non-ferrous alloy with a 10 mm diameter and 50 mm gauge length - Leaving Cert Engineering - Question b - 2020

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The results shown below were obtained from a tensile test on a non-ferrous alloy with a 10 mm diameter and 50 mm gauge length. | Load (kN) | 15 | 25 | 40 | 60 |... show full transcript

Worked Solution & Example Answer:The results shown below were obtained from a tensile test on a non-ferrous alloy with a 10 mm diameter and 50 mm gauge length - Leaving Cert Engineering - Question b - 2020

Step 1

Using the graph paper supplied, plot the load-extension diagram.

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Answer

  1. On the x-axis, label the extension in mm, ranging from 0 to 1.5 mm.
  2. On the y-axis, label the load in kN, ranging from 0 to 120 kN.
  3. Plot each pair of values from the table on the graph:
    • (0.06 mm, 15 kN)
    • (0.10 mm, 25 kN)
    • (0.16 mm, 40 kN)
    • (0.26 mm, 60 kN)
    • (0.38 mm, 80 kN)
    • (0.65 mm, 100 kN)
    • (0.90 mm, 107 kN)
    • (1.00 mm, 108 kN)
    • (1.20 mm, 95 kN)
    • (1.40 mm, 96 kN)
  4. Connect the points to form a smooth curve.

Step 2

Indicate each of the following regions on your graph: Elastic region

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  1. The Elastic Region is typically from the origin to the point where the curve begins to deviate linearly. Mark this region on the graph.

Step 3

Indicate each of the following regions on your graph: Plastic region

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  1. The Plastic Region is where the material deforms permanently. Mark the section of the curve after the elastic region that continues to rise but begins to flatten.

Step 4

Indicate each of the following regions on your graph: Necking region

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  1. The Necking Region occurs after the maximum load is reached, where the curve starts to drop. Mark this area on the graph.

Step 5

Determine the ultimate tensile strength (UTS) of the alloy in kN/mm².

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Answer

The Ultimate Tensile Strength (UTS) can be calculated using the formula:

extUTS=Max LoadC.S.A. ext{UTS} = \frac{\text{Max Load}}{\text{C.S.A.}}

The maximum load observed is 108 kN, and the circular cross-sectional area (C.S.A.) of the alloy is given by:

C.S.A.=π(d2)2=π(5)2=25πmm2\text{C.S.A.} = \pi\left(\frac{d}{2}\right)^{2} = \pi(5)^{2} = 25\pi \, \text{mm}^{2}

Using these values, we calculate:

UTS=108 kN25π mm21.38 kN/mm2\text{UTS} = \frac{108 \text{ kN}}{25\pi \, \text{ mm}^{2}} \approx 1.38 \text{ kN/mm}^{2}

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