OCR MEI M2 2006 January — Question 3 20 marks

Exam BoardOCR MEI
ModuleM2 (Mechanics 2)
Year2006
SessionJanuary
Marks20
PaperDownload PDF ↗
Mark schemeDownload PDF ↗
TopicCentre of Mass 1
TypeParticle attached to lamina - find mass/position
DifficultyStandard +0.3 This is a standard M2 centre of mass question with routine composite lamina calculations and a straightforward optimization. Part (a) involves standard techniques (moments about axes, removing a section), while part (b) is basic framework statics with moment equilibrium and resolution of forces. All methods are textbook-standard with no novel insight required, making it slightly easier than average.
Spec6.04b Find centre of mass: using symmetry6.04c Composite bodies: centre of mass

3
  1. A uniform lamina made from rectangular parts is shown in Fig. 3.1. All the dimensions are centimetres. All coordinates are referred to the axes shown in Fig. 3.1. \begin{figure}[h]
    \includegraphics[alt={},max width=\textwidth]{c1785fde-a6ce-4f8b-9948-4b4dd973ce84-4_691_529_427_762} \captionsetup{labelformat=empty} \caption{Fig. 3.1}
    \end{figure}
    1. Show that the \(x\)-coordinate of the centre of mass of the lamina is 6.5 and find the \(y\)-coordinate. A square of side 2 cm is to be cut from the lamina. The sides of the square are to be parallel to the coordinate axes and the centre of the square is to be chosen so that the \(x\)-coordinate of the centre of mass of the new shape is 6.4
    2. Calculate the \(x\)-coordinate of the centre of the square to be removed. The \(y\)-coordinate of the centre of the square to be removed is now chosen so that the \(y\)-coordinate of the centre of mass of the final shape is as large as possible.
    3. Calculate the \(y\)-coordinate of the centre of mass of the lamina with the square removed, giving your answer correct to three significant figures.
  2. Fig. 3.2 shows a framework made from light rods of length 2 m freely pin-jointed at \(\mathrm { A } , \mathrm { B } , \mathrm { C }\), D and E. The framework is in a vertical plane and is supported at A and C. There are loads of 120 N at B and at E . The force on the framework due to the support at A is \(R \mathrm {~N}\). \begin{figure}[h]
    \includegraphics[alt={},max width=\textwidth]{c1785fde-a6ce-4f8b-9948-4b4dd973ce84-5_448_741_459_662} \captionsetup{labelformat=empty} \caption{Fig. 3.2}
    \end{figure} each rod is 2 m long
    1. Show that \(R = 150\).
    2. Draw a diagram showing all the forces acting at the points \(\mathrm { A } , \mathrm { B } , \mathrm { D }\) and E , including the forces internal to the rods. Calculate the internal forces in rods AE and EB , and determine whether each is a tension or a thrust. [You may leave your answers in surd form.]
    3. Without any further calculation of the forces in the rods, explain briefly how you can tell that rod ED is in thrust.

Question 3:
Part (a)(i)
AnswerMarks Guidance
AnswerMark Guidance
\(80\begin{pmatrix}\bar{x}\\\bar{y}\end{pmatrix} = 48\begin{pmatrix}6\\2\end{pmatrix} + 12\begin{pmatrix}1\\-3\end{pmatrix} + 20\begin{pmatrix}11\\9\end{pmatrix}\)M1 Correct method for c.m.
\(80\begin{pmatrix}\bar{x}\\\bar{y}\end{pmatrix} = \begin{pmatrix}520\\240\end{pmatrix}\)B1 Total mass correct
B1One c.m. on RHS correct [If separate components considered, B1 for 2 correct]
\(\bar{x} = 6.5\)E1
\(\bar{y} = 3\)A1 cao
Part (a)(ii)
AnswerMarks Guidance
AnswerMark Guidance
Consider \(x\) coordinate: \(520 = 76 \times 6.4 + 4x\)M1 Using additive principle o.e. on \(x\) components
B1Areas correct. Allow FT from masses from (i)
so \(x = 8.4\)A1 cao
Part (a)(iii)
AnswerMarks Guidance
AnswerMark Guidance
\(y\) coordinate is 1 so we need \(240 = 76\bar{y} + 4 \times 1\) and \(\bar{y} = 3.10526...\)B1 Position of centre of square
M1
so 3.11 (3 s.f.)A1 cao
Part (b)(i)
AnswerMarks Guidance
AnswerMark Guidance
Moments about C: \(4R = 120 \times 3 + 120 \times 2\)M1 Moments equation. All terms present
so \(4R = 600\) and \(R = 150\)E1
Part (b)(ii)
AnswerMarks Guidance
AnswerMark Guidance
[Diagram showing framework with forces]B1
A\(\uparrow\): \(150 + T_{AE}\cos 30 = 0\)M1 Equilibrium at a pin-joint
\(T_{AE} = -100\sqrt{3}\) so \(100\sqrt{3}\) N (C)A1 Any form. Sign correct. Neglect (C)
E\(\downarrow\): \(120 + T_{AE}\cos 30 + T_{EB}\cos 30 = 0\)M1 Equilibrium at E, all terms present
\(T_{EB} = 20\sqrt{3}\) so \(20\sqrt{3}\) N (T)F1 Any form. Sign follows working. Neglect (T).
F1T/C consistent with answers
Part (b)(iii)
AnswerMarks Guidance
AnswerMark Guidance
Consider \(\rightarrow\) at E, using (ii) gives ED as thrustE1 Clearly explained. Accept 'thrust' correctly deduced from wrong answers to (ii).
# Question 3:

## Part (a)(i)

| Answer | Mark | Guidance |
|--------|------|----------|
| $80\begin{pmatrix}\bar{x}\\\bar{y}\end{pmatrix} = 48\begin{pmatrix}6\\2\end{pmatrix} + 12\begin{pmatrix}1\\-3\end{pmatrix} + 20\begin{pmatrix}11\\9\end{pmatrix}$ | M1 | Correct method for c.m. |
| $80\begin{pmatrix}\bar{x}\\\bar{y}\end{pmatrix} = \begin{pmatrix}520\\240\end{pmatrix}$ | B1 | Total mass correct |
| | B1 | One c.m. on RHS correct [If separate components considered, B1 for 2 correct] |
| $\bar{x} = 6.5$ | E1 | |
| $\bar{y} = 3$ | A1 | cao |

## Part (a)(ii)

| Answer | Mark | Guidance |
|--------|------|----------|
| Consider $x$ coordinate: $520 = 76 \times 6.4 + 4x$ | M1 | Using additive principle o.e. on $x$ components |
| | B1 | Areas correct. Allow FT from masses from (i) |
| so $x = 8.4$ | A1 | cao |

## Part (a)(iii)

| Answer | Mark | Guidance |
|--------|------|----------|
| $y$ coordinate is 1 so we need $240 = 76\bar{y} + 4 \times 1$ and $\bar{y} = 3.10526...$ | B1 | Position of centre of square |
| | M1 | |
| so 3.11 (3 s.f.) | A1 | cao |

## Part (b)(i)

| Answer | Mark | Guidance |
|--------|------|----------|
| Moments about C: $4R = 120 \times 3 + 120 \times 2$ | M1 | Moments equation. All terms present |
| so $4R = 600$ and $R = 150$ | E1 | |

## Part (b)(ii)

| Answer | Mark | Guidance |
|--------|------|----------|
| [Diagram showing framework with forces] | B1 | |
| A$\uparrow$: $150 + T_{AE}\cos 30 = 0$ | M1 | Equilibrium at a pin-joint |
| $T_{AE} = -100\sqrt{3}$ so $100\sqrt{3}$ N (C) | A1 | Any form. Sign correct. Neglect (C) |
| E$\downarrow$: $120 + T_{AE}\cos 30 + T_{EB}\cos 30 = 0$ | M1 | Equilibrium at E, all terms present |
| $T_{EB} = 20\sqrt{3}$ so $20\sqrt{3}$ N (T) | F1 | Any form. Sign follows working. Neglect (T). |
| | F1 | T/C consistent with answers |

## Part (b)(iii)

| Answer | Mark | Guidance |
|--------|------|----------|
| Consider $\rightarrow$ at E, using (ii) gives ED as thrust | E1 | Clearly explained. Accept 'thrust' correctly deduced from wrong answers to (ii). |

---
3
\begin{enumerate}[label=(\alph*)]
\item A uniform lamina made from rectangular parts is shown in Fig. 3.1. All the dimensions are centimetres. All coordinates are referred to the axes shown in Fig. 3.1.

\begin{figure}[h]
\begin{center}
  \includegraphics[alt={},max width=\textwidth]{c1785fde-a6ce-4f8b-9948-4b4dd973ce84-4_691_529_427_762}
\captionsetup{labelformat=empty}
\caption{Fig. 3.1}
\end{center}
\end{figure}
\begin{enumerate}[label=(\roman*)]
\item Show that the $x$-coordinate of the centre of mass of the lamina is 6.5 and find the $y$-coordinate.

A square of side 2 cm is to be cut from the lamina. The sides of the square are to be parallel to the coordinate axes and the centre of the square is to be chosen so that the $x$-coordinate of the centre of mass of the new shape is 6.4
\item Calculate the $x$-coordinate of the centre of the square to be removed.

The $y$-coordinate of the centre of the square to be removed is now chosen so that the $y$-coordinate of the centre of mass of the final shape is as large as possible.
\item Calculate the $y$-coordinate of the centre of mass of the lamina with the square removed, giving your answer correct to three significant figures.
\end{enumerate}\item Fig. 3.2 shows a framework made from light rods of length 2 m freely pin-jointed at $\mathrm { A } , \mathrm { B } , \mathrm { C }$, D and E. The framework is in a vertical plane and is supported at A and C. There are loads of 120 N at B and at E . The force on the framework due to the support at A is $R \mathrm {~N}$.

\begin{figure}[h]
\begin{center}
  \includegraphics[alt={},max width=\textwidth]{c1785fde-a6ce-4f8b-9948-4b4dd973ce84-5_448_741_459_662}
\captionsetup{labelformat=empty}
\caption{Fig. 3.2}
\end{center}
\end{figure}

each rod is 2 m long
\begin{enumerate}[label=(\roman*)]
\item Show that $R = 150$.
\item Draw a diagram showing all the forces acting at the points $\mathrm { A } , \mathrm { B } , \mathrm { D }$ and E , including the forces internal to the rods.

Calculate the internal forces in rods AE and EB , and determine whether each is a tension or a thrust. [You may leave your answers in surd form.]
\item Without any further calculation of the forces in the rods, explain briefly how you can tell that rod ED is in thrust.
\end{enumerate}\end{enumerate}

\hfill \mbox{\textit{OCR MEI M2 2006 Q3 [20]}}