What Is the Resultant Velocity of an Airplane in Wind?

AI Thread Summary
The discussion focuses on calculating the resultant velocity of an airplane with an airspeed of 420 km/h at a 45-degree angle and a westward wind speed of 30 km/h. Participants suggest using vector addition to break down the velocities into their x and y components for clarity. The wind acts as a headwind, affecting the airplane's speed in the direction it's traveling. By applying trigonometric functions, specifically using the cosine of the angle, the effective wind speed can be calculated and subtracted from the airplane's airspeed. Ultimately, this approach leads to the correct resultant velocity of approximately 399 km/h.
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An airplane has an air speed of 4.20 × 10^2 km/h [N 45° E]. The wind speed is 30 km/h
to the west.

a) What is the airplane’s resultant velocity?

I decided to use the trigonometric solution, but I am confused on how to break the equation down in order to get 399 km/h

c2 = a2 + b2 - 2ab.cosC
c2 = (4.20 x 10^2)^2 + (30)^2 - 2( 420) x (30)cos135
c2 = (17640000 + 900) - 17819
c2 = 17623081
c2 = ? (I tried square root of 17623081, but of course this is far off from the answer)

Please assist!
 
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You're on the right track with the trigonometric approach, but you went about it wrong. The initial velocity you have is 4.2 x 10^2 at an angle of 45 degrees North of East. Isn't your c term the 4.2 x 10^2?
From here you have a wind slowing down the x direction of the plane.
The velocity you have now is incorporating both the x and y directions. How can you divide the velocity up so you can deal with the x and y directions separately?
 
Hmm.. I am not sure what you mean. I am terrible at this! I don`t know the velocity (the 339 km/h is the answer I am suppose to find) so how would I divide it up?
 
Yes, but I am not sure if I am doing it correctly.
Would a = 420 km/h [N 45 E] + b = 30 km/h [W] equals the resultant? But, when drawing it, at what angle would 30 km/h [W] be?
 
Draw it.

You will see it's a simple case of a 30 km/h headwind at 45 degrees off the plane's nose.

So the effect of the headwind along the path of the plane will be 30*cos (45). Subtract that from 420 and you have your answer.

You can use trig if you like - but a bit of thought will often save you having to remember complicated formulae.
 
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