The plane's drift angle is (a) [tex]5.89^o[/tex]
The given parameters are:
[tex]S_p = 350m/h[/tex] --- the speed of the plane
[tex]S_w = 40m/h[/tex] --- the speed of the wind
[tex]d_p = N40^oE[/tex] ---- the direction of the plane
[tex]d_w = S70^oE[/tex] ---- the direction of the wind
Start by resolving the components of the motion of the plane and of the wind, as follows:
[tex]S_p=350 \times \sin(40)i +350 \times \cos(40)j[/tex] ---- for the plane
[tex]S_p=224.98i +268.12j[/tex]
[tex]S_w=40 \times \sin(70)i -40 \times \cos(70)j[/tex] --- for the wind
[tex]S_w=37.59i -13.68j[/tex]
Add the resolution of vectors
[tex]S = S_p + S_w[/tex]
[tex]S = 224.98i + 37.59i + 268.12j - 13.68j[/tex]
[tex]S = 262.57i + 254.44j[/tex]
Next, we calculate the plane's direction as follows:
[tex]\theta = \tan^{-1}(\frac{262.57}{254.44})[/tex]
[tex]\theta = 45.90^o[/tex]
Rewrite as:
[tex]\theta = N45.90^oE[/tex]
The drift angle is then calculated as:
[tex]D = \theta -d_p[/tex]
This gives
[tex]D = N45.90^oE - N40^oE[/tex]
[tex]D = N5.90^oE[/tex]
Rewrite as:
[tex]D = 5.90^o[/tex]
Hence, the plane's drift angle is (a) [tex]5.89^o[/tex]
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