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FIGURE 7.1 below shows a beam subjected to three point loads - NSC Mechanical Technology Welding and Metalwork - Question 7 - 2023 - Paper 1

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FIGURE 7.1 below shows a beam subjected to three point loads. 7.1.1 Calculate the magnitude of the reactions at RL and RR. 7.1.2 Calculate the bending moments at ... show full transcript

Worked Solution & Example Answer:FIGURE 7.1 below shows a beam subjected to three point loads - NSC Mechanical Technology Welding and Metalwork - Question 7 - 2023 - Paper 1

Step 1

7.1.1 Calculate the magnitude of the reactions at RL and RR.

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Answer

To find the reactions at points RL and RR, we will take moments about one end of the beam to eliminate the reaction at that end.

  1. Taking Moments about RL:

    Moment = 0 = RR * 7 m - (4 N * 1.5 m) - (5 N * (3.5 m)) - (3 N * (5.5 m))

    After solving, we get: RR=5.71NRR = 5.71 N

  2. Taking Moments about RR:

    Moment = 0 = RL * 7 m - (3 N * 1.5 m) - (5 N * (3.5 m)) - (4 N * (5.5 m))

    After solving, we find: RL=6.29NRL = 6.29 N

Step 2

7.1.2 Calculate the bending moments at points A, B and C.

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Answer

The bending moment at points A, B, and C can be calculated as:

  1. Bending Moment at A (BM_A):

    BMA=RL1.54N1.5=6.29N1.54N1.5=9.44NmBM_A = RL * 1.5 - 4 N * 1.5 = 6.29 N * 1.5 - 4 N * 1.5 = 9.44 Nm

  2. Bending Moment at B (BM_B):

    BMB=RL3.54N1.55N2=6.29N3.54N1.55N2=14.02NmBM_B = RL * 3.5 - 4 N * 1.5 - 5 N * 2 = 6.29 N * 3.5 - 4 N * 1.5 - 5 N * 2 = 14.02 Nm

  3. Bending Moment at C (BM_C):

    BMC=RL5.54N1.55N3.53N(2m)=6.29N5.54N1.55N3.53N2=8.60NmBM_C = RL * 5.5 - 4 N * 1.5 - 5 N * 3.5 - 3 N * (2 m) = 6.29 N * 5.5 - 4 N * 1.5 - 5 N * 3.5 - 3 N * 2 = 8.60 Nm

Step 3

7.1.3 Draw a bending-moment diagram.

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Answer

To draw the bending-moment diagram, we plot the bending moments calculated at points A, B, and C on a vertical axis against their respective positions along the beam on a horizontal axis. The scale used for the diagram will be consistent, such as 1 mm = 2 Nm. The diagram will depict the values:

  • BM_A = 9.44 Nm
  • BM_B = 14.02 Nm
  • BM_C = 8.60 Nm

The resulting graph should form a triangular shape, illustrating how the bending moments change along the length of the beam.

Step 4

7.2.1 The area of the bar.

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Answer

To calculate the area (A) of the round aluminium bar, use the formula:

A=FσA = \frac{F}{\sigma}

Where:

  • F=65kN=65×103NF = 65 kN = 65 \times 10^3 N
  • σ=5MPa=5×106N/m2\sigma = 5 MPa = 5 \times 10^6 N/m^2

Substituting in the values:

A=65×1035×106=0.013m2=13×103m2A = \frac{65 \times 10^3}{5 \times 10^6} = 0.013 m^2 = 13 \times 10^{-3} m^2

Step 5

7.2.2 The diameter of the bar.

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Answer

The diameter (D) of the bar can be calculated using the area:

A=πD24A = \frac{\pi D^2}{4}

Rearranging gives:

D=4AπD = \sqrt{\frac{4A}{\pi}}

Substituting A=13×103m2A = 13 \times 10^{-3} m^2:

D=4×13×103π=0.1267mD128.66 mmD = \sqrt{\frac{4 \times 13 \times 10^{-3}}{\pi}} = 0.1267 m \\ D \approx 128.66 \ mm

Step 6

7.2.3 The strain.

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Answer

Strain (ϵ\epsilon) is defined as:

ϵ=ΔLL0\epsilon = \frac{\Delta L}{L_0}

Using Young's modulus to relate stress and strain:

σ=Eϵ\sigma = E \cdot \epsilon

Where:

  • E=75×109E = 75 \times 10^9 Pa

Thus:

ϵ=σE=5×10675×109=6.67×105\epsilon = \frac{\sigma}{E} = \frac{5 \times 10^6}{75 \times 10^9} = 6.67 \times 10^{-5}

Step 7

7.2.4 The change in length.

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Answer

The change in length (ΔL\Delta L) can be calculated using:

ΔL=ϵL0\Delta L = \epsilon \cdot L_0

Where:

  • L0=250mm=0.25mL_0 = 250 mm = 0.25 m

Thus: ΔL=6.67×1050.25=0.000016675m=0.02mm\Delta L = 6.67 \times 10^{-5} \cdot 0.25 = 0.000016675 m = 0.02 mm

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