| Exam Board | CAIE |
|---|---|
| Module | Further Paper 3 (Further Paper 3) |
| Year | 2023 |
| Session | June |
| Marks | 7 |
| Paper | Download PDF ↗ |
| Mark scheme | Download PDF ↗ |
| Topic | Centre of Mass 1 |
| Type | Lamina with removed triangle/rectangle/square |
| Difficulty | Standard +0.8 This is a standard Further Maths mechanics problem requiring composite body centre of mass calculation using the removal method, followed by applying the toppling condition. While it involves multiple steps (finding centroids of triangles, using the composite formula, then applying equilibrium), the techniques are routine for FM students and the geometry is straightforward with a right-angled triangle. The algebraic manipulation is moderate but not particularly challenging. |
| Spec | 6.04c Composite bodies: centre of mass6.04e Rigid body equilibrium: coplanar forces |
| Answer | Marks |
|---|---|
| 3(a) | [Mass is proportional to area] |
| Answer | Marks | Guidance |
|---|---|---|
| 2 | B1 | All correct for ABC and DEC. |
| Answer | Marks | Guidance |
|---|---|---|
| 2 3 2 | M1 | All moment terms present, dimensionally correct, |
| Answer | Marks |
|---|---|
| A1 | All correct moments about AC. |
| Answer | Marks | Guidance |
|---|---|---|
| 348a5x | A1 | AEF |
| Answer | Marks |
|---|---|
| Area | Centre of mass |
| Answer | Marks |
|---|---|
| ABC | 1 |
| Answer | Marks |
|---|---|
| 2 | 2a |
| DEC | 1 |
| Answer | Marks |
|---|---|
| 2 | 1 |
| Answer | Marks |
|---|---|
| ADEB | 5 |
| Answer | Marks | Guidance |
|---|---|---|
| 2 | x | |
| Question | Answer | Marks |
| Answer | Marks |
|---|---|
| 3(b) | 288a2 5x2 |
| Answer | Marks | Guidance |
|---|---|---|
| 348a5x | B1 FT | FT their expression for x from part (a). |
| Rearrange to 3-term quadratic: 10x2 144ax288a2 0 | M1 | Allow 3-term inequality. |
| Answer | Marks | Guidance |
|---|---|---|
| 5 | A1 | Single correct answer, no inequality, CWO. |
| Answer | Marks | Guidance |
|---|---|---|
| Question | Answer | Marks |
Question 3:
--- 3(a) ---
3(a) | [Mass is proportional to area]
Area Centre of mass
from AC
ABC 1 2a
.6a.8a (24a2)
2
DEC 1 1
x.5a x
2 3
ADEB 5 x
24a2 xa
2 | B1 | All correct for ABC and DEC.
5 1 5
Moments [about AC] x 24a2 xa 24a22a x ax
2 3 2 | M1 | All moment terms present, dimensionally correct,
allow sign error.
A1 | All correct moments about AC.
288a2 5x2
x
348a5x | A1 | AEF
4
Area | Centre of mass
from AC
ABC | 1
.6a.8a (24a2)
2 | 2a
DEC | 1
x.5a
2 | 1
x
3
ADEB | 5
24a2 xa
2 | x
Question | Answer | Marks | Guidance
--- 3(b) ---
3(b) | 288a2 5x2
On the point of toppling about E: x x, x
348a5x | B1 FT | FT their expression for x from part (a).
Rearrange to 3-term quadratic: 10x2 144ax288a2 0 | M1 | Allow 3-term inequality.
25x12ax12a0,
12
x a
5 | A1 | Single correct answer, no inequality, CWO.
3
Question | Answer | Marks | Guidance
\includegraphics{figure_3}
A uniform lamina is in the form of a triangle $ABC$, with $AC = 8a$, $BC = 6a$ and angle $ACB = 90°$. The point $D$ on $AC$ is such that $AD = 3a$. The point $E$ on $CB$ is such that $CE = x$ (see diagram). The triangle $CDE$ is removed from the lamina.
\begin{enumerate}[label=(\alph*)]
\item Find, in terms of $a$ and $x$, the distance of the centre of mass of the remaining object $ADEB$ from $AC$. [4]
\end{enumerate}
The object $ADEB$ is on the point of toppling about the point $E$ when the object is in the vertical plane with its edge $EB$ on a smooth horizontal surface.
\begin{enumerate}[label=(\alph*)]
\setcounter{enumi}{1}
\item Find $x$ in terms of $a$. [3]
\end{enumerate}
\hfill \mbox{\textit{CAIE Further Paper 3 2023 Q3 [7]}}