1999 Paper 2 Q11

Year: 1999
Paper: 2
Question Number: 11

Course: UFM Mechanics
Section: Circular Motion 1

Difficulty: 1600.0 Banger: 1484.0

Problem

An automated mobile dummy target for gunnery practice is moving anti-clockwise around the circumference of a large circle of radius \(R\) in a horizontal plane at a constant angular speed \(\omega\). A shell is fired from \(O\), the centre of this circle, with initial speed \(V\) and angle of elevation \(\alpha\). Show that if \(V^2 < gR\), then no matter what the value of \(\alpha\), or what vertical plane the shell is fired in, the shell cannot hit the target. Assume now that \(V^2 > gR\) and that the shell hits the target, and let \(\beta\) be the angle through which the target rotates between the time at which the shell is fired and the time of impact. Show that \(\beta\) satisfies the equation $$ g^2{{\beta}^4} - 4{{\omega}^2}{V^2}{{\beta}^2} +4{R^2}{{\omega}^4}=0. $$ Deduce that there are exactly two possible values of \(\beta\). Let \(\beta_1\) and \(\beta_2\) be the possible values of \(\beta\) and let \(P_1\) and \(P_2\) be the corresponding points of impact. By considering the quantities \((\beta_1^2 +\beta_2^2) \) and \(\beta_1^2\beta_2^2\,\), or otherwise, show that the linear distance between \(P_1\) and \(P_2\) is \[ 2R \sin\Big( \frac\omega g \sqrt{V^2-Rg}\Big) \;. \]

Solution

\begin{align*} && 0 &= V\sin \alpha t-\frac12 gt^2 \\ \Rightarrow && t &= \frac{2V \sin \alpha}{g} \\ && R &= V \cos \alpha \, t \\ &&&= \frac{2V^2 \sin \alpha \cos \alpha}{g} \\ &&&= \frac{V^2 \sin 2 \alpha}{g} \end{align*} Therefore the max distance is \(\frac{V^2}{g}\), therefore we cannot hit the target if \(R > \frac{V^2}{g} \Rightarrow gR > V^2\). We have \(\beta = \omega t \Rightarrow t = \frac{\beta}{\omega}\) \begin{align*} && \sin \alpha &= \frac{gt}{2V} \\ && \cos \alpha &= \frac{R}{Vt} \\ \Rightarrow && 1 &= \left (\frac{gt}{2V} \right)^2 + \left ( \frac{R}{Vt} \right)^2 \\ &&&= \left (\frac{g\beta}{2V \omega} \right)^2 + \left ( \frac{R\omega}{V\beta} \right)^2 \\ &&&= \frac{g^2 \beta^2}{4 V^2 \omega^2} + \frac{R^2 \omega^2}{V^2 \beta ^2} \\ \Rightarrow && 4V^2 \omega^2 \beta^2 &= g^2 \beta^4 + 4R^2 \omega^4 \\ \Rightarrow && 0 &= g^2 \beta^4 - 4\omega^2 V^2 \beta^2+4R^2\omega^4 \end{align*} This (quadratic) equation in terms of \(\beta^2\) has two solution if \(\Delta = 16\omega^4V^4-16g^2R^2\omega^4 =16\omega^4(V^4-g^2R^2) > 0\) since \(V^2 > gR\). Since \(\beta > 0\) there are exactly two solutions, once we have values for \(\beta\). First notice, \begin{align*} && \beta_1^2 + \beta_2^2 &= \frac{4\omega^2V^2}{g^2} \\ && \beta_1^2\beta_2^2 &= \frac{4R^2\omega^4}{g^2} \end{align*} Then notice the positions of \(P_1\) and \(P_2\) are \((R\cos \beta_1 , R\sin \beta_1)\) and \((R\cos \beta_2, R\sin \beta_2)\). \begin{align*} && d^2 &= R^2\left ( \cos \beta_1 - \cos \beta_2 \right)^2 + R^2 \left ( \sin \beta_1 - \sin \beta_2 \right)^2 \\ &&&= 2R^2 - 2R^2(\cos \beta_1 \cos \beta_2 + \sin \beta_1 \sin \beta_2) \\ &&&= 2R^2-2R^2\cos(\beta_1 - \beta_2) \\ &&&= 2R^2 \left (1-\cos(\sqrt{(\beta_1-\beta_2)^2} \right ) \\ &&&= 2R^2 \left (1 - \cos\left ( \sqrt{\frac{4\omega^2 V^2}{g^2} - \frac{4R\omega^2}{g}} \right) \right) \\ &&&= 2R^2 \left (1 - \cos\left (\frac{2\omega}{g} \sqrt{V^2 - Rg} \right) \right) \\ &&&= 4 R^2 \sin^2 \left (\frac{\omega}{g} \sqrt{V^2 - Rg} \right) \end{align*} which gives us the required result.
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Difficulty Rating: 1600.0

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Banger Rating: 1484.0

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Problem source
An automated mobile dummy target for gunnery practice is moving anti-clockwise around the circumference of a large circle of radius $R$ in a horizontal plane at a constant angular speed $\omega$.  
A shell is fired from $O$, the centre of this circle, with initial speed $V$ and angle of elevation $\alpha$.  
Show that if $V^2 < gR$, then no matter what the value of $\alpha$, or what vertical plane the shell is fired in, the shell cannot hit the target.
Assume now that $V^2 > gR$ and that the shell hits the target, and let $\beta$ be the angle through which the target rotates between the time at which the shell is fired and the time of impact. Show that $\beta$ satisfies the equation
$$
g^2{{\beta}^4} - 4{{\omega}^2}{V^2}{{\beta}^2}
+4{R^2}{{\omega}^4}=0.
$$
Deduce that there are exactly two possible values of $\beta$. Let $\beta_1$ and $\beta_2$ be the possible values of $\beta$ and let $P_1$ and $P_2$ be the corresponding points of impact.
By considering the quantities $(\beta_1^2 +\beta_2^2) $ and $\beta_1^2\beta_2^2\,$, or otherwise, show that the linear distance between $P_1$ and $P_2$ is
\[
2R \sin\Big( \frac\omega g \sqrt{V^2-Rg}\Big) 
\;.
\]
Solution source
\begin{align*}
&& 0 &= V\sin \alpha t-\frac12 gt^2 \\
\Rightarrow && t &= \frac{2V \sin \alpha}{g} \\
&& R &= V \cos \alpha \, t \\
&&&= \frac{2V^2 \sin \alpha \cos \alpha}{g} \\
&&&= \frac{V^2 \sin 2 \alpha}{g}
\end{align*}

Therefore the max distance is $\frac{V^2}{g}$, therefore we cannot hit the target if $R > \frac{V^2}{g} \Rightarrow gR > V^2$.

We have $\beta = \omega t \Rightarrow t = \frac{\beta}{\omega}$

\begin{align*}
&& \sin \alpha &= \frac{gt}{2V} \\
&& \cos \alpha &= \frac{R}{Vt} \\
\Rightarrow && 1 &= \left (\frac{gt}{2V} \right)^2 + \left ( \frac{R}{Vt}  \right)^2 \\
&&&=  \left (\frac{g\beta}{2V \omega} \right)^2 + \left ( \frac{R\omega}{V\beta}  \right)^2 \\
&&&= \frac{g^2 \beta^2}{4 V^2 \omega^2} + \frac{R^2 \omega^2}{V^2 \beta ^2} \\
\Rightarrow && 4V^2 \omega^2 \beta^2 &= g^2 \beta^4 + 4R^2 \omega^4 \\
\Rightarrow && 0 &= g^2 \beta^4 - 4\omega^2 V^2 \beta^2+4R^2\omega^4
\end{align*}

This (quadratic) equation in terms of $\beta^2$ has two solution if $\Delta = 16\omega^4V^4-16g^2R^2\omega^4 =16\omega^4(V^4-g^2R^2) > 0$ since $V^2 > gR$.

Since $\beta > 0$ there are exactly two solutions, once we have values for $\beta$.

First notice, 

\begin{align*}
&& \beta_1^2 + \beta_2^2 &= \frac{4\omega^2V^2}{g^2} \\
&& \beta_1^2\beta_2^2 &= \frac{4R^2\omega^4}{g^2}
\end{align*} 

Then notice the positions of $P_1$ and $P_2$ are $(R\cos \beta_1 , R\sin \beta_1)$ and $(R\cos \beta_2, R\sin \beta_2)$. 

\begin{align*}
&& d^2 &= R^2\left ( \cos \beta_1 - \cos \beta_2 \right)^2 + R^2 \left ( \sin \beta_1 - \sin \beta_2 \right)^2 \\
&&&= 2R^2 - 2R^2(\cos \beta_1 \cos \beta_2 + \sin \beta_1 \sin \beta_2) \\
&&&= 2R^2-2R^2\cos(\beta_1 - \beta_2) \\
&&&= 2R^2 \left (1-\cos(\sqrt{(\beta_1-\beta_2)^2} \right ) \\
&&&= 2R^2 \left (1 - \cos\left ( \sqrt{\frac{4\omega^2 V^2}{g^2} - \frac{4R\omega^2}{g}} \right) \right) \\
&&&= 2R^2 \left (1 - \cos\left (\frac{2\omega}{g} \sqrt{V^2 - Rg} \right) \right) \\
&&&= 4 R^2 \sin^2 \left (\frac{\omega}{g} \sqrt{V^2 - Rg} \right)
\end{align*}

which gives us the required result.