Respuesta :
vx=-200cos60+60cos25
vy=-200sin60+60sin25
v=(vx^2+vy^2)^(1/2)
v=154.73mph
tana=vy/vx
a=arctan(vy/vx)
a≈72.85 and this is in the third quadrant so:
The bearing is 180+72.85=252.85
So:
The plane is traveling at a speed of 154.73mph with a bearing of 252.85°
vy=-200sin60+60sin25
v=(vx^2+vy^2)^(1/2)
v=154.73mph
tana=vy/vx
a=arctan(vy/vx)
a≈72.85 and this is in the third quadrant so:
The bearing is 180+72.85=252.85
So:
The plane is traveling at a speed of 154.73mph with a bearing of 252.85°
Answer:
<154.72, 197.15 degrees> (D)
Step-by-step explanation:
First we turn bearings into workable angles:
Bearing to angle = 90 - θ
Airplane bearing to angle = 90 - 240 = -150 = 210 (add 360 to -150)
Wind bearing to angle = 90 - 25 = 65
Now let's work on the vectors of the plane and the wind
Airplane vector: <200cos(210), 200sin(210)> = <-173.2,-100>
Wind vector: <60cos(65), 60sin(65)> = <25.36, 54.38>
Add the two to get the component form of the actual speed vector and we get:
<-147.84, -45.62>
Trig form: <sqrt(h^2+v^2), arctan(v/h)>
<sqrt(147.84^2+45.62^2), arctan(v/h)> = <154.72, 197.15 degrees>
*the trig form shows that u = <speed, angle>
Let me know if I missed anything; was kind of in a rush.