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A tensile force of 25 kN is applied to a rectangular bar 12 mm thick and 22 mm wide. The original length is 1,8 m and Young's modulus for the steel is 195 GPa. Calculate the following: The stress, The final length of the bar.

Physics

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QUESTION 6: STRESS, STRAIN AND YOUNG'S MODULUS

6.1 A tensile force of 25 kN is applied to a rectangular bar 12 mm thick and 22 mm wide. The original length is 1,8 m and Young's modulus for the steel is 195 GPa.

Given:

  • Force F=25 kN=25×103 NF = 25 \text{ kN} = 25 \times 10^3 \text{ N}
  • Thickness t=12 mm=0.012 mt = 12 \text{ mm} = 0.012 \text{ m}
  • Width w=22 mm=0.022 mw = 22 \text{ mm} = 0.022 \text{ m}
  • Original length L0=1.8 mL_0 = 1.8 \text{ m}
  • Young's modulus E=195 GPa=195×109 PaE = 195 \text{ GPa} = 195 \times 10^9 \text{ Pa}
6.1.1 The stress
  1. Calculate the cross-sectional area of the bar.

    A=w×t=0.022 m×0.012 m=0.000264 m2A = w \times t = 0.022 \text{ m} \times 0.012 \text{ m} = 0.000264 \text{ m}^2
  2. Calculate the stress (σ\sigma).

    σ=FA\sigma = \frac{F}{A} σ=25×103 N0.000264 m2\sigma = \frac{25 \times 10^3 \text{ N}}{0.000264 \text{ m}^2} σ≈94.6969×106 Pa\sigma \approx 94.6969 \times 10^6 \text{ Pa} σ≈94.70 MPa\sigma \approx 94.70 \text{ MPa}

    The stress is 94.70 MPa\boxed{\text{94.70 MPa}}.

    6.1.2 The final length of the bar
  3. Calculate the strain (ϵ\epsilon).

    ϵ=σE\epsilon = \frac{\sigma}{E} ϵ=94.6969×106 Pa195×109 Pa\epsilon = \frac{94.6969 \times 10^6 \text{ Pa}}{195 \times 10^9 \text{ Pa}} ϵ≈0.0004856\epsilon \approx 0.0004856
  4. Calculate the change in length (ΔL\Delta L).

    ΔL=ϵ×L0\Delta L = \epsilon \times L_0 ΔL=0.0004856×1.8 m\Delta L = 0.0004856 \times 1.8 \text{ m} ΔL≈0.00087408 m\Delta L \approx 0.00087408 \text{ m}
  5. Calculate the final length (LfL_f).

    Lf=L0+ΔLL_f = L_0 + \Delta L Lf=1.8 m+0.00087408 mL_f = 1.8 \text{ m} + 0.00087408 \text{ m} Lf≈1.80087 mL_f \approx 1.80087 \text{ m}

    The final length of the bar is 1.80087 m\boxed{\text{1.80087 m}}.

    6.2 FIGURE 3 below shows a round steel rod subjected to a tensile load of 55 kN. Young's modulus for the steel is 200 GPa.

    Given:

    • Tensile load F=55 kN=55×103 NF = 55 \text{ kN} = 55 \times 10^3 \text{ N}
    • Young's modulus E=200 GPa=200×109 PaE = 200 \text{ GPa} = 200 \times 10^9 \text{ Pa}
    • Section 1: Diameter D1=25 mm=0.025 mD_1 = 25 \text{ mm} = 0.025 \text{ m}, Length L1=100 mm=0.1 mL_1 = 100 \text{ mm} = 0.1 \text{ m}
    • Section 2: Diameter D2=50 mm=0.050 mD_2 = 50 \text{ mm} = 0.050 \text{ m}, Length L2=100 mm=0.1 mL_2 = 100 \text{ mm} = 0.1 \text{ m}
  6. Calculate the cross-sectional areas of both sections.

    A1=πD124=π(0.025 m)24=π×0.0006254≈0.00049087 m2A_1 = \frac{\pi D_1^2}{4} = \frac{\pi (0.025 \text{ m})^2}{4} = \frac{\pi \times 0.000625}{4} \approx 0.00049087 \text{ m}^2 A2=πD224=π(0.050 m)24=π×0.00254≈0.0019635 m2A_2 = \frac{\pi D_2^2}{4} = \frac{\pi (0.050 \text{ m})^2}{4} = \frac{\pi \times 0.0025}{4} \approx 0.0019635 \text{ m}^2
    6.2.1 The maximum tensile stress
  7. The maximum tensile stress occurs in the section with the smallest cross-sectional area (Section 1).

    σmax=FA1\sigma_{max} = \frac{F}{A_1} σmax=55×103 N0.00049087 m2\sigma_{max} = \frac{55 \times 10^3 \text{ N}}{0.00049087 \text{ m}^2} σmax≈112.04×106 Pa\sigma_{max} \approx 112.04 \times 10^6 \text{ Pa} σmax≈112.04 MPa\sigma_{max} \approx 112.04 \text{ MPa}

    The maximum tensile stress is 112.04 MPa\boxed{\text{112.04 MPa}}.

    6.2.2 The minimum stress in the rod
  8. The minimum stress occurs in the section with the largest cross-sectional area (Section 2).

    σmin=FA2\sigma_{min} = \frac{F}{A_2} σmin=55×103 N0.0019635 m2\sigma_{min} = \frac{55 \times 10^3 \text{ N}}{0.0019635 \text{ m}^2} σmin≈28.01×106 Pa\sigma_{min} \approx 28.01 \times 10^6 \text{ Pa} σmin≈28.01 MPa\sigma_{min} \approx 28.01 \text{ MPa}

    The minimum stress in the rod is 28.01 MPa\boxed{\text{28.01 MPa}}.

    6.2.3 The total strain

    The question likely refers to the total elongation (change in length) of the rod, as "total strain" for a composite bar is ambiguous.

  9. Calculate the strain and elongation for Section 1.

    ϵ1=σmaxE=112.04×106 Pa200×109 Pa≈0.0005602\epsilon_1 = \frac{\sigma_{max}}{E} = \frac{112.04 \times 10^6 \text{ Pa}}{200 \times 10^9 \text{ Pa}} \approx 0.0005602 ΔL1=ϵ1×L1=0.0005602×0.1 m=0.00005602 m\Delta L_1 = \epsilon_1 \times L_1 = 0.0005602 \times 0.1 \text{ m} = 0.00005602 \text{ m}
  10. Calculate the strain and elongation for Section 2.

    ϵ2=σminE=28.01×106 Pa200×109 Pa≈0.00014005\epsilon_2 = \frac{\sigma_{min}}{E} = \frac{28.01 \times 10^6 \text{ Pa}}{200 \times 10^9 \text{ Pa}} \approx 0.00014005 ΔL2=ϵ2×L2=0.00014005×0.1 m=0.000014005 m\Delta L_2 = \epsilon_2 \times L_2 = 0.00014005 \times 0.1 \text{ m} = 0.000014005 \text{ m}
  11. Calculate the total elongation.

    ΔLtotal=ΔL1+ΔL2\Delta L_{total} = \Delta L_1 + \Delta L_2 ΔLtotal=0.00005602 m+0.000014005 m\Delta L_{total} = 0.00005602 \text{ m} + 0.000014005 \text{ m} ΔLtotal=0.000070025 m\Delta L_{total} = 0.000070025 \text{ m}

    The total elongation (change in length) is 0.000070025 m\boxed{\text{0.000070025 m}}.

    QUESTION 7: HEAT

    7.1 Describe the isothermal process.

    An isothermal process is a thermodynamic process in which the temperature of the system remains constant throughout. Any heat transfer into or out of the system occurs slowly enough to maintain thermal equilibrium.

    7.2 A right rectangular prism of cast iron has dimensions of 55×45×35 mm55 \times 45 \times 35 \text{ mm} at 25∘C25^\circ \text{C}. The prism is heated to 88∘C88^\circ \text{C}. The coefficient of linear expansion of cast iron is 9×10−6/∘C9 \times 10^{-6} /^\circ \text{C}.

    Given:

    • Initial dimensions: L0=55 mmL_0 = 55 \text{ mm}, W0=45 mmW_0 = 45 \text{ mm}, H0=35 mmH_0 = 35 \text{ mm}
    • Initial temperature T1=25∘CT_1 = 25^\circ \text{C}
    • Final temperature T2=88∘CT_2 = 88^\circ \text{C}
    • Coefficient of linear expansion α=9×10−6/∘C\alpha = 9 \times 10^{-6} /^\circ \text{C}
  12. Calculate the initial volume (V0V_0) of the prism.

    V0=L0×W0×H0V_0 = L_0 \times W_0 \times H_0 V0=55 mm×45 mm×35 mmV_0 = 55 \text{ mm} \times 45 \text{ mm} \times 35 \text{ mm} V0=86625 mm3V_0 = 86625 \text{ mm}^3
  13. Calculate the change in temperature (ΔT\Delta T).

    ΔT=T2−T1=88∘C−25∘C=63∘C\Delta T = T_2 - T_1 = 88^\circ \text{C} - 25^\circ \text{C} = 63^\circ \text{C}
  14. Calculate the coefficient of volumetric expansion (γ\gamma).

    γ=3α=3×(9×10−6/∘C)=27×10−6/∘C\gamma = 3\alpha = 3 \times (9 \times 10^{-6} /^\circ \text{C}) = 27 \times 10^{-6} /^\circ \text{C}
    7.2.1 The increase in volume
  15. Calculate the increase in volume (ΔV\Delta V).

    ΔV=V0γΔT\Delta V = V_0 \gamma \Delta T ΔV=(86625 mm3)(27×10−6/∘C)(63∘C)\Delta V = (86625 \text{ mm}^3)(27 \times 10^{-6} /^\circ \text{C})(63^\circ \text{C}) ΔV=86625×0.000027×63 mm3\Delta V = 86625 \times 0.000027 \times 63 \text{ mm}^3 ΔV≈147.34 mm3\Delta V \approx 147.34 \text{ mm}^3

    The increase in volume is 147.34 mm3\boxed{\text{147.34 mm}^3}.

    7.2.2 The volume at 88∘C88^\circ \text{C}
  16. Calculate the final volume (VfV_f).

    Vf=V0+ΔVV_f = V_0 + \Delta V Vf=86625 mm3+147.34 mm3V_f = 86625 \text{ mm}^3 + 147.34 \text{ mm}^3 Vf=86772.34 mm3V_f = 86772.34 \text{ mm}^3

    The volume at 88∘C88^\circ \text{C} is 86772.34 mm3\boxed{\text{86772.34 mm}^3}.

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