binbagsss
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An aeroplane (A) can fly at 600kmh^-1 in still air. It has to fly to an airport which is SW of its current position. There is a wind of 90kmh^-1 blowing from N20W.
a) Find the direction that the plane should take relative to the wind
b) what is the ground speed of aeroplane.
I have attached two diagrams. The difference only being the bearing on which I draw the velocity of the wind.
Diagram 2, where I take the the negative of VW- changing the bearing to S20W is the correct one. What is the exact reason for this?
I have also noticed that whichever diagram I use, lead me to calculate angle x as the same in either case, so the answer to part a in this question, (sin x = sin (130-x) - sin 65 = sin 115)
however that the way in which I chose to draw the diagram determines angle y - via the sine rule determining also the ground speed of the aeroplane.
Help as to why diagram 2 is the correct way is greatly appreciated.
One more thing that I do not quite understand is the direction of aVw in diagram 2. On the diagram to me this looks like : - (-Va) + Vw = Va+ Vw, but I always thought that the direction of this must be in line with Va - Vw.
(as this was drawn through reversing Va initially)
Thanks for any assistance much appreciated !
(Apologies on the diagrams, units to all velocities are kmh^-1 , Va - velocity of aeroplane , VW - velocity of wind.)
a) Find the direction that the plane should take relative to the wind
b) what is the ground speed of aeroplane.
I have attached two diagrams. The difference only being the bearing on which I draw the velocity of the wind.
Diagram 2, where I take the the negative of VW- changing the bearing to S20W is the correct one. What is the exact reason for this?
I have also noticed that whichever diagram I use, lead me to calculate angle x as the same in either case, so the answer to part a in this question, (sin x = sin (130-x) - sin 65 = sin 115)
however that the way in which I chose to draw the diagram determines angle y - via the sine rule determining also the ground speed of the aeroplane.
Help as to why diagram 2 is the correct way is greatly appreciated.
One more thing that I do not quite understand is the direction of aVw in diagram 2. On the diagram to me this looks like : - (-Va) + Vw = Va+ Vw, but I always thought that the direction of this must be in line with Va - Vw.
(as this was drawn through reversing Va initially)
Thanks for any assistance much appreciated !
(Apologies on the diagrams, units to all velocities are kmh^-1 , Va - velocity of aeroplane , VW - velocity of wind.)