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Question 6
7.1.1 Calculate the reactions at RL and RR. 7.1.2 Calculate the bending moments at points B, C and D. 7.1.3 Construct the bending moment diagram for points B, C an... show full transcript
Step 1
Answer
To find the reactions at supports RL and RR, we can use the equilibrium equations. The sum of vertical forces must equal zero.
Let R_L and R_R be the reactions at supports.
The total downward load is
.
Setting up the equilibrium equations:
.
Taking moments about point R_L:
.
Calculating:
\Rightarrow 680 = R_R imes 8\ \Rightarrow R_R = 85 ext{ N}$$. Substituting for R_R: $$R_L = 240 - 85 = 155 ext{ N}$$. Thus, the reactions are: - R_L = 155 N - R_R = 85 NStep 2
Answer
The bending moments at points B, C, and D can be calculated using the moments established from the reactions and loads applied.
At Point B:
.
At Point C:
.
At Point D:
\Rightarrow 1085 - 400 - 120 = 565 ext{ Nm}$$.
Step 3
Answer
To construct the bending moment diagram:
Establish a scale suitable for the values obtained; for instance, use 1 cm for 1 m and 0.1 Nm for 1 cm.
Mark the calculated moments on the horizontal line representing the length of the bar from A to E.
Plot points:
Connect these points with straight lines, ensuring to reflect any changes in moment due to loads.
The diagram should visually represent the variation of bending moments along the structure.
Step 4
Answer
Using the tensile stress formula:
A = rac{40,000}{20 imes 10^6} = 0.002 m^2$$. The area of a circle is $A = rac{ ext{π}}{4} d^2$, so: $$rac{ ext{π}}{4} d^2 = 0.002\ \Rightarrow d^2 = rac{0.002 imes 4}{ ext{π}}\ \Rightarrow d = rac{4 imes 0.002}{ ext{π}}^{0.5}\ \Rightarrow d = 0.0503 ext{ m} ext{ or } 50.3 ext{ mm}$$.Step 5
Answer
Strain is calculated as:
\Rightarrow ext{Change in Length} = ext{Stress} imes rac{ ext{Length}}{E}$$, where E (Young's modulus) = 90 GPa = 90 imes 10^9 Pa: $$ ext{Change in Length} = rac{20 imes 10^6 imes 2}{90 imes 10^9} = 0.00044444 ext{ m} = 0.44444 ext{ mm}$$. Substituting: $$ ext{Strain} = rac{0.4444 imes 10^{-3}}{2} ightarrow 0.00022222$$.Step 6
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