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QUESTION 7: STRESS, STRAIN AND YOUNG'S MODULUS A copper rod that is 5,2 m long is subjected to a tensile load of 850 kg. The rod elongates by 1,25 mm.

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QUESTION 7: STRESS, STRAIN AND YOUNG'S MODULUS

7.1 A copper rod that is 5,2 m long is subjected to a tensile load of 850 kg. The rod elongates by 1,25 mm.

Given:

  • Original length, L=5.2 mL = 5.2 \text{ m}
  • Mass of load, m=850 kgm = 850 \text{ kg}
  • Elongation, ΔL=1.25 mm=0.00125 m\Delta L = 1.25 \text{ mm} = 0.00125 \text{ m}
  • Acceleration due to gravity, g=9.81 m/s2g = 9.81 \text{ m/s}^2

Assumption: The original diameter of the copper rod is 16 mm16 \text{ mm}, as provided in the context of Question 7.2 for a gauge length section, and no other diameter is given for 7.1.

  • Original diameter, D=16 mm=0.016 mD = 16 \text{ mm} = 0.016 \text{ m}
  1. Calculate the tensile force (FF).

    F=mg=(850 kg)(9.81 m/s2)=8338.5 NF = mg = (850 \text{ kg})(9.81 \text{ m/s}^2) = 8338.5 \text{ N}
  2. Calculate the cross-sectional area (AA).

    A=πD24=π(0.016 m)24=0.000064π m2≈2.0106×10−4 m2A = \frac{\pi D^2}{4} = \frac{\pi (0.016 \text{ m})^2}{4} = 0.000064\pi \text{ m}^2 \approx 2.0106 \times 10^{-4} \text{ m}^2

    7.1.1 Calculate the tensile stress on the rod.

  3. Calculate the tensile stress (σ\sigma).

    σ=FA=8338.5 N2.0106×10−4 m2≈41472697 Pa\sigma = \frac{F}{A} = \frac{8338.5 \text{ N}}{2.0106 \times 10^{-4} \text{ m}^2} \approx 41472697 \text{ Pa} σ≈41.47 MPa\sigma \approx 41.47 \text{ MPa}

    The tensile stress on the rod is 41.47 MPa\boxed{\text{41.47 MPa}}.

    7.1.2 Calculate the strain on the rod.

  4. Calculate the strain (ϵ\epsilon).

    ϵ=ΔLL=0.00125 m5.2 m≈0.00024038\epsilon = \frac{\Delta L}{L} = \frac{0.00125 \text{ m}}{5.2 \text{ m}} \approx 0.00024038

    The strain on the rod is 0.000240\boxed{\text{0.000240}}.

    7.2 The following data were recorded during a tensile test on a steel specimen:

    Given:

    • Original diameter, D0=16 mm=0.016 mD_0 = 16 \text{ mm} = 0.016 \text{ m}
    • Gauge length, L0=80 mm=0.080 mL_0 = 80 \text{ mm} = 0.080 \text{ m}
    • Gauge length at fracture, Lf=92.16 mmL_f = 92.16 \text{ mm}
    • Neck diameter at fracture, Df=11.52 mmD_f = 11.52 \text{ mm}
  5. Calculate the original cross-sectional area (A0A_0).

    A0=πD024=π(0.016 m)24=0.000064π m2≈2.0106×10−4 m2A_0 = \frac{\pi D_0^2}{4} = \frac{\pi (0.016 \text{ m})^2}{4} = 0.000064\pi \text{ m}^2 \approx 2.0106 \times 10^{-4} \text{ m}^2
  6. Calculate Stress and Strain for each data point.

    • Stress (σ=LoadA0\sigma = \frac{\text{Load}}{A_0})
    • Strain (ϵ=ExtensionL0\epsilon = \frac{\text{Extension}}{L_0})
    Load (kN)Load (N)Extension (mm)Extension (m)Stress (σ\sigma) (MPa)Strain (ϵ\epsilon)
    000000
    15150000.01820.000018274.600.0002275
    30300000.03630.0000363149.210.00045375
    45450000.05470.0000547223.820.00068375
    60600000.07240.0000724298.420.000905
    75750000.09100.0000910373.030.0011375

    7.2.1 Draw a stress-strain graph for these values.

    (Due to the text-based format, I cannot draw the graph. However, the table above provides the calculated stress and strain values needed to plot the graph. The graph should have strain on the x-axis and stress on the y-axis. The points should be plotted and connected to form the stress-strain curve. The tip suggests a scale of 10 mm=10 MPa10 \text{ mm} = 10 \text{ MPa} for stress and 10 mm=50×10−610 \text{ mm} = 50 \times 10^{-6} for strain.)

    7.2.2 Determine Young's modulus of elasticity with the aid of the graph.

  7. Determine Young's Modulus (EE) from the linear elastic region.

    Young's Modulus is the slope of the stress-strain graph in the elastic region. We can use any two points from the linear part of the table (e.g., from Load 15 kN to Load 60 kN).
    Let's use the points corresponding to 15 kN and 60 kN:

    • Point 1: (ϵ1,σ1)=(0.0002275,74.60 MPa)(\epsilon_1, \sigma_1) = (0.0002275, 74.60 \text{ MPa})
    • Point 2: (ϵ2,σ2)=(0.000905,298.42 MPa)(\epsilon_2, \sigma_2) = (0.000905, 298.42 \text{ MPa})
    E=ΔσΔϵ=σ2−σ1ϵ2−ϵ1E = \frac{\Delta \sigma}{\Delta \epsilon} = \frac{\sigma_2 - \sigma_1}{\epsilon_2 - \epsilon_1} E=(298.42−74.60)×106 Pa(0.000905−0.0002275)E = \frac{(298.42 - 74.60) \times 10^6 \text{ Pa}}{(0.000905 - 0.0002275)} E=223.82×106 Pa0.0006775≈330361623 PaE = \frac{223.82 \times 10^6 \text{ Pa}}{0.0006775} \approx 330361623 \text{ Pa} E≈330.36 GPaE \approx 330.36 \text{ GPa}

    Young's modulus of elasticity is 330.36 GPa\boxed{\text{330.36 GPa}}.

    7.2.3 Determine the percentage reduction in area.

  8. Calculate the final cross-sectional area (AfA_f).

    Af=πDf24=π(0.01152 m)24=0.00010432896π m2≈1.0433×10−4 m2A_f = \frac{\pi D_f^2}{4} = \frac{\pi (0.01152 \text{ m})^2}{4} = 0.00010432896\pi \text{ m}^2 \approx 1.0433 \times 10^{-4} \text{ m}^2
  9. Calculate the percentage reduction in area.

    Percentage reduction in area=A0−AfA0×100%\text{Percentage reduction in area} = \frac{A_0 - A_f}{A_0} \times 100\% Percentage reduction in area=2.0106×10−4 m2−1.0433×10−4 m22.0106×10−4 m2×100%\text{Percentage reduction in area} = \frac{2.0106 \times 10^{-4} \text{ m}^2 - 1.0433 \times 10^{-4} \text{ m}^2}{2.0106 \times 10^{-4} \text{ m}^2} \times 100\% Percentage reduction in area=0.9673×10−42.0106×10−4×100%≈48.11%\text{Percentage reduction in area} = \frac{0.9673 \times 10^{-4}}{2.0106 \times 10^{-4}} \times 100\% \approx 48.11\%

    The percentage reduction in area is 48.11%\boxed{\text{48.11\%}}.

    7.3 A hollow steel tube has an outside diameter of 50 mm and an inside diameter of 30 mm. The tube is 3,8 m long and is subjected to an axial tensile load of 60 kN.

    Given:

    • Outside diameter, Do=50 mm=0.050 mD_o = 50 \text{ mm} = 0.050 \text{ m}
    • Inside diameter, Di=30 mm=0.030 mD_i = 30 \text{ mm} = 0.030 \text{ m}
    • Length, L=3.8 mL = 3.8 \text{ m}
    • Axial tensile load, F=60 kN=60000 NF = 60 \text{ kN} = 60000 \text{ N}
  10. Calculate the cross-sectional area (AA) of the hollow tube.

    A=π4(Do2−Di2)=π4((0.050 m)2−(0.030 m)2)A = \frac{\pi}{4}(D_o^2 - D_i^2) = \frac{\pi}{4}((0.050 \text{ m})^2 - (0.030 \text{ m})^2) A=π4(0.0025−0.0009) m2=π4(0.0016) m2=0.0004π m2≈1.2566×10−3 m2A = \frac{\pi}{4}(0.0025 - 0.0009) \text{ m}^2 = \frac{\pi}{4}(0.0016) \text{ m}^2 = 0.0004\pi \text{ m}^2 \approx 1.2566 \times 10^{-3} \text{ m}^2

    7.3.1 Calculate the normal stress in the tube.

  11. Calculate the normal stress (σ\sigma).

    σ=FA=60000 N0.0004π m2≈47746482.9 Pa\sigma = \frac{F}{A} = \frac{60000 \text{ N}}{0.0004\pi \text{ m}^2} \approx 47746482.9 \text{ Pa} σ≈47.75 MPa\sigma \approx 47.75 \text{ MPa}

    The normal stress in the tube is 47.75 MPa\boxed{\text{47.75 MPa}}.

    7.3.2 If the extension of the tube is 0,76 mm, calculate the strain.

    Given:

    • Elongation, ΔL=0.76 mm=0.00076 m\Delta L = 0.76 \text{ mm} = 0.00076 \text{ m}
  12. Calculate the strain (ϵ\epsilon).

    ϵ=ΔLL=0.00076 m3.8 m=0.0002\epsilon = \frac{\Delta L}{L} = \frac{0.00076 \text{ m}}{3.8 \text{ m}} = 0.0002

    The strain is 0.0002\boxed{\text{0.0002}}.

    7.3.3 Determine Young's modulus of the material.

  13. Determine Young's Modulus (EE).

    E=σϵ=47.746×106 Pa0.0002≈238730000000 PaE = \frac{\sigma}{\epsilon} = \frac{47.746 \times 10^6 \text{ Pa}}{0.0002} \approx 238730000000 \text{ Pa} E≈238.73 GPaE \approx 238.73 \text{ GPa}

    Young's modulus of the material is 238.73 GPa\boxed{\text{238.73 GPa}}.

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