FIGURE 7.1 below shows a beam subjected to three point loads - NSC Mechanical Technology Welding and Metalwork - Question 7 - 2023 - Paper 1
Question 7
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.
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=5.71N
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=6.29N
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:
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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=σF
Where:
F=65kN=65×103N
σ=5MPa=5×106N/m2
Substituting in the values:
A=5×10665×103=0.013m2=13×10−3m2
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=4πD2
Rearranging gives:
D=π4A
Substituting A=13×10−3m2:
D=π4×13×10−3=0.1267mD≈128.66mm
Step 6
7.2.3 The strain.
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Strain (ϵ) is defined as:
ϵ=L0ΔL
Using Young's modulus to relate stress and strain:
σ=E⋅ϵ
Where:
E=75×109 Pa
Thus:
ϵ=Eσ=75×1095×106=6.67×10−5
Step 7
7.2.4 The change in length.
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The change in length (ΔL) can be calculated using: