Edexcel M4 2004 June — Question 1 6 marks

Exam BoardEdexcel
ModuleM4 (Mechanics 4)
Year2004
SessionJune
Marks6
PaperDownload PDF ↗
Mark schemeDownload PDF ↗
TopicVectors Introduction & 2D
TypeRelative velocity: find resultant velocity (magnitude and/or direction)
DifficultyStandard +0.3 This is a standard M4 relative velocity problem requiring vector addition and component resolution. Part (a) involves equating j-components (routine), and part (b) requires finding the magnitude of the resultant velocity vector. While it needs careful notation and understanding of relative velocity, it follows a well-established method with no novel insight required, making it slightly easier than average.
Spec1.10a Vectors in 2D: i,j notation and column vectors1.10b Vectors in 3D: i,j,k notation1.10e Position vectors: and displacement1.10h Vectors in kinematics: uniform acceleration in vector form

  1. \hspace{0pt} [In this question \(\mathbf { i }\) and \(\mathbf { j }\) are horizontal unit vectors due east and due north respectively.]
An aeroplane makes a journey from a point \(P\) to a point \(Q\) which is due east of \(P\). The wind velocity is \(w ( \cos \theta \mathbf { i } + \sin \theta \mathbf { j } )\), where \(w\) is a positive constant. The velocity of the aeroplane relative to the wind is \(v ( \cos \phi \mathbf { i } - \sin \phi \mathbf { j } )\), where \(v\) is a constant and \(v > w\). Given that \(\theta\) and \(\phi\) are both acute angles,
  1. show that \(v \sin \phi = w \sin \theta\),
  2. find, in terms of \(v , w\) and \(\theta\), the speed of the aeroplane relative to the ground.

\begin{enumerate}
  \item \hspace{0pt} [In this question $\mathbf { i }$ and $\mathbf { j }$ are horizontal unit vectors due east and due north respectively.]
\end{enumerate}

An aeroplane makes a journey from a point $P$ to a point $Q$ which is due east of $P$. The wind velocity is $w ( \cos \theta \mathbf { i } + \sin \theta \mathbf { j } )$, where $w$ is a positive constant. The velocity of the aeroplane relative to the wind is $v ( \cos \phi \mathbf { i } - \sin \phi \mathbf { j } )$, where $v$ is a constant and $v > w$. Given that $\theta$ and $\phi$ are both acute angles,\\
(a) show that $v \sin \phi = w \sin \theta$,\\
(b) find, in terms of $v , w$ and $\theta$, the speed of the aeroplane relative to the ground.\\

\hfill \mbox{\textit{Edexcel M4 2004 Q1 [6]}}