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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. 7.1.1 Calculate the tensile stress on the rod. 7.1.2 Calculate the strain on the rod.

Physics

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QUESTION 7: STRESS, STRAIN AND YOUNG'S MODULUS

7.1.1 Calculate the tensile stress on the rod.

  1. Calculate the tensile force FF.

    The mass m=850 kgm = 850 \text{ kg}.
    The acceleration due to gravity g=9.8 m/s2g = 9.8 \text{ m/s}^2.

    F=mg=850 kg×9.8 m/s2=8330 NF = mg = 850 \text{ kg} \times 9.8 \text{ m/s}^2 = 8330 \text{ N}
  2. State the formula for tensile stress.

    Tensile stress σ=FA\sigma = \frac{F}{A}, where FF is the tensile force and AA is the cross-sectional area of the rod.
    Note: The cross-sectional area of the copper rod is not provided in the question. Therefore, a numerical value for the tensile stress cannot be calculated.
    The tensile force is 8330 N\boxed{8330 \text{ N}}.

    7.1.2 Calculate the strain on the rod.

  3. Identify the original length and the elongation.

    Original length L=5.2 mL = 5.2 \text{ m}.
    Elongation ΔL=1.25 mm=0.00125 m\Delta L = 1.25 \text{ mm} = 0.00125 \text{ m}.

  4. Calculate the strain ϵ\epsilon using the formula ϵ=ΔLL\epsilon = \frac{\Delta L}{L}.

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

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

    7.2.1 Draw a stress strain graph for these values.

  5. Calculate the original cross-sectional area A0A_0.

    Original diameter D0=16 mm=0.016 mD_0 = 16 \text{ mm} = 0.016 \text{ m}.

    A0=πD024=π(0.016 m)24=π×0.000256 m24=0.000064π m2≈2.0106×10−4 m2A_0 = \frac{\pi D_0^2}{4} = \frac{\pi (0.016 \text{ m})^2}{4} = \frac{\pi \times 0.000256 \text{ m}^2}{4} = 0.000064\pi \text{ m}^2 \approx 2.0106 \times 10^{-4} \text{ m}^2
  6. Calculate the stress (σ=LoadA0\sigma = \frac{\text{Load}}{A_0}) and strain (ϵ=ExtensionL0\epsilon = \frac{\text{Extension}}{L_0}) for each data point.

    Gauge length L0=80 mm=0.080 mL_0 = 80 \text{ mm} = 0.080 \text{ m}.

    Load (kN)Extension (mm)Stress (σ=Load/A0\sigma = \text{Load}/A_0) (MPa)Strain (ϵ=Extension/L0\epsilon = \text{Extension}/L_0)
    0000
    150.018215×1032.0106×10−4≈74.60\frac{15 \times 10^3}{2.0106 \times 10^{-4}} \approx 74.600.018280=0.0002275\frac{0.0182}{80} = 0.0002275
    300.036330×1032.0106×10−4≈149.21\frac{30 \times 10^3}{2.0106 \times 10^{-4}} \approx 149.210.036380=0.00045375\frac{0.0363}{80} = 0.00045375
    450.054745×1032.0106×10−4≈223.91\frac{45 \times 10^3}{2.0106 \times 10^{-4}} \approx 223.910.054780=0.00068375\frac{0.0547}{80} = 0.00068375
    600.072460×1032.0106×10−4≈298.42\frac{60 \times 10^3}{2.0106 \times 10^{-4}} \approx 298.420.072480=0.000905\frac{0.0724}{80} = 0.000905
    750.091075×1032.0106×10−4≈373.02\frac{75 \times 10^3}{2.0106 \times 10^{-4}} \approx 373.020.091080=0.0011375\frac{0.0910}{80} = 0.0011375
  7. Describe how to draw the graph.

    Plot the calculated stress values on the y-axis and the strain values on the x-axis. Use the given scale: 10 mm=10 MPa10 \text{ mm} = 10 \text{ MPa} for the stress axis and 10 mm=50×10−610 \text{ mm} = 50 \times 10^{-6} for the strain axis. The points should form a roughly linear relationship, representing the elastic region of the material.
    (As an AI, I cannot physically draw the graph, but the table above provides the necessary data points for plotting.)

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

  8. Young's modulus EE is the slope of the linear portion of the stress-strain graph.

    We can calculate it using any point in the elastic region (e.g., the last data point before yielding, assuming the given data is within the elastic range).
    Using the last data point: σ=373.02 MPa\sigma = 373.02 \text{ MPa} and ϵ=0.0011375\epsilon = 0.0011375.

    E=σϵ=373.02×106 Pa0.0011375E = \frac{\sigma}{\epsilon} = \frac{373.02 \times 10^6 \text{ Pa}}{0.0011375} E≈3.279×1011 Pa=327.9 GPaE \approx 3.279 \times 10^{11} \text{ Pa} = 327.9 \text{ GPa}

    Young's modulus of elasticity is 327.9 GPa\boxed{327.9 \text{ GPa}}.

    7.2.3 Determine the percentage reduction in area.

  9. Calculate the original area A0A_0 and the final area AfA_f.

    Original diameter D0=16 mmD_0 = 16 \text{ mm}.
    Neck diameter at fracture Df=11.52 mmD_f = 11.52 \text{ mm}.

    A0=πD024=π(16 mm)24=64π mm2A_0 = \frac{\pi D_0^2}{4} = \frac{\pi (16 \text{ mm})^2}{4} = 64\pi \text{ mm}^2 Af=πDf24=π(11.52 mm)24=π×132.7104 mm24=33.1776π mm2A_f = \frac{\pi D_f^2}{4} = \frac{\pi (11.52 \text{ mm})^2}{4} = \frac{\pi \times 132.7104 \text{ mm}^2}{4} = 33.1776\pi \text{ mm}^2
  10. 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=64π mm2−33.1776π mm264π mm2×100%\text{Percentage reduction in area} = \frac{64\pi \text{ mm}^2 - 33.1776\pi \text{ mm}^2}{64\pi \text{ mm}^2} \times 100\% Percentage reduction in area=64−33.177664×100%\text{Percentage reduction in area} = \frac{64 - 33.1776}{64} \times 100\% Percentage reduction in area=30.822464×100%=0.4816×100%=48.16%\text{Percentage reduction in area} = \frac{30.8224}{64} \times 100\% = 0.4816 \times 100\% = 48.16\%

    The percentage reduction in area is 48.16%\boxed{48.16\%}.

    7.3.1 Calculate the normal stress in the tube.

  11. Calculate the cross-sectional area AA of the hollow tube.

    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}.

    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 m2−0.0009 m2)=π4(0.0016 m2)=0.0004π m2≈1.2566×10−3 m2A = \frac{\pi}{4}(0.0025 \text{ m}^2 - 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
  12. Calculate the normal stress σ\sigma using the formula σ=FA\sigma = \frac{F}{A}.

    Axial tensile load F=60 kN=60×103 NF = 60 \text{ kN} = 60 \times 10^3 \text{ N}.

    σ=60×103 N0.0004π m2\sigma = \frac{60 \times 10^3 \text{ N}}{0.0004\pi \text{ m}^2} σ≈47746482.9 Pa≈47.75 MPa\sigma \approx 47746482.9 \text{ Pa} \approx 47.75 \text{ MPa}

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

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

  13. Identify the original length and the extension.

    Original length L=3.8 mL = 3.8 \text{ m}.
    Extension ΔL=0.76 mm=0.00076 m\Delta L = 0.76 \text{ mm} = 0.00076 \text{ m}.

  14. Calculate the strain ϵ\epsilon using the formula ϵ=ΔLL\epsilon = \frac{\Delta L}{L}.

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

    The strain is 0.0002\boxed{0.0002}.

    7.3.3 Determine Young's modulus of the material.

  15. Use the calculated stress from 7.3.1 and strain from 7.3.2.

    Stress σ=47.75 MPa=47.75×106 Pa\sigma = 47.75 \text{ MPa} = 47.75 \times 10^6 \text{ Pa}.
    Strain ϵ=0.0002\epsilon = 0.0002.

  16. Calculate Young's modulus EE using the formula E=σϵE = \frac{\sigma}{\epsilon}.

    E=47.75×106 Pa0.0002E = \frac{47.75 \times 10^6 \text{ Pa}}{0.0002} E=238.75×109 Pa=238.75 GPaE = 238.75 \times 10^9 \text{ Pa} = 238.75 \text{ GPa}

    Young's modulus of the material is 238.75 GPa\boxed{238.75 \text{ GPa}}.

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