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Question: Air speed of an airplane is \(400km{{h}^{-1}}\). The wind is blowing at \(200km{{h}^{-1}}\) towards ...

Air speed of an airplane is 400kmh1400km{{h}^{-1}}. The wind is blowing at 200kmh1200km{{h}^{-1}} towards east direction. In what direction should the pilot try to fly the plane so as to move exactly towards the north east.

Explanation

Solution

The flow of the wind will affect the motion of the plane. The resultant velocity of the plane will be equal to the vector sum of the airspeed of the plane and the velocity of the wind. Draw a vector diagram and find the angle that the pilot should make for the required condition.

Complete step by step answer:
When an airplane flies in presence of a wind, the speed and direction of the wind affects the motion of the plane. The wind may either assist the motion of the plane or oppose the motion of the plane depending upon the speed and direction of the wind.In this case, the wind is blowing with a speed of 200kmh1200km{{h}^{-1}} towards east. This will increase the speed of the plane by 200kmh1200km{{h}^{-1}} towards east. Let the initial direction of the plane be making an angle θ\theta with horizontal and the plane will move with a speed of 400kmh1400km{{h}^{-1}}. Due to this the resultant velocity of the plane will be equal to the vector sum of the airspeed of the plane and the velocity of the wind, as shown in the figure.

Here, VA{{V}_{A}} is the airspeed of the plane, VW{{V}_{W}} is the velocity of the wind and VR{{V}_{R}} is the resultant velocity of the plane.

Since VR{{V}_{R}} is resultant of VA{{V}_{A}} and VW{{V}_{W}}, the vertical component of the VR{{V}_{R}} is equal to sum of the vertical components of the VA{{V}_{A}} and VW{{V}_{W}}.
i.e. VR2=VAsinθ\dfrac{{{V}_{R}}}{\sqrt{2}}={{V}_{A}}\sin \theta .…. (i)
And the horizontal component of VR{{V}_{R}} is equal to sum of the horizontal components of the VA{{V}_{A}} and VW{{V}_{W}}.
i.e. VR2=VAcosθ+VW\dfrac{{{V}_{R}}}{\sqrt{2}}={{V}_{A}}\cos \theta +{{V}_{W}} ….. (ii).
Now, equate (i) and (ii).
VAsinθ=VAcosθ+VW\Rightarrow {{V}_{A}}\sin \theta ={{V}_{A}}\cos \theta +{{V}_{W}}
VAsinθVAcosθ=VW\Rightarrow {{V}_{A}}\sin \theta -{{V}_{A}}\cos \theta ={{V}_{W}}
Substitute VA=400kmh1{{V}_{A}}=400km{{h}^{-1}} and VW=200kmh1{{V}_{W}}=200km{{h}^{-1}}.
400sinθ400cosθ=200\Rightarrow 400\sin \theta -400\cos \theta =200
sinθcosθ=12\Rightarrow \sin \theta -\cos \theta =\dfrac{1}{2}
Divide the equation by cos45=12\cos {{45}^{\circ }}=\dfrac{1}{\sqrt{2}}.
sinθcos45cosθcos45=122\Rightarrow \sin \theta \cos {{45}^{\circ }}-\cos \theta \cos {{45}^{\circ }}=\dfrac{1}{2\sqrt{2}}
But from trigonometry we know that,
sinθcos45cosθcos45=sin(θ45)\sin \theta \cos {{45}^{\circ }}-\cos \theta \cos {{45}^{\circ }}=\sin (\theta -{{45}^{\circ }}).
Then,
sin(θ45)=122\Rightarrow \sin (\theta -{{45}^{\circ }})=\dfrac{1}{2\sqrt{2}}
θ45=sin1122\Rightarrow \theta -{{45}^{\circ }}={{\sin }^{-1}}\dfrac{1}{2\sqrt{2}}
θ45=20.7\Rightarrow \theta -{{45}^{\circ }}={{20.7}^{\circ }}
θ=20.7+45=65.7\therefore \theta ={{20.7}^{\circ }}+{{45}^{\circ }}={{65.7}^{\circ }}

Therefore, in order to fly the plane towards north-east, the pilot must try to fly the plane in the direction that makes an angle of 65.7{{65.7}^{\circ }} with a positive x-axis.

Note: In order to solve direction problems students may be confused in direction. So always remember below chart

And always assume all distances to be along straight lines and between specified points each main direction changes north to west /east, it will be 9090{}^\circ change but the change between north and north east is only 4545{}^\circ .