Answer:
(a). The components of the velocity of the jet airliner relative to the air is
[tex]v_{JA_{x}}=3.10\times10^{2}\ mi/h[/tex]
[tex]v_{JA_{y}}=0[/tex]
(b). The components of the velocity of the air relative to earth is
[tex]v_{AE_{x}}=0.90\times10^{2}\ mi/h[/tex]
[tex]v_{AE_{y}}=0.41\times10^{2}\ mi/h[/tex]
Explanation:
Given that,
Initial speed of jet [tex]v_{i}=3.10\times10^{2}\ mi/h[/tex]
Speed of wind = 1.00\times10^{2}\ mi/h[/tex]
Angle = 24.5°
(a). We need to calculate the components of the velocity of the jet airliner relative to the air,
Using formula of velocity
The components of the velocity
[tex]v_{JA_{x}}=3.10\times10^{2}\ mi/h[/tex]
[tex]v_{JA_{y}}=0[/tex]
(b). We need to calculate the components of the velocity of the air relative to earth,
Using formula of the components of the velocity
For x-axis,
[tex]v_{AE_{x}}=v_{w}\cos\theta[/tex]
Put the value into the formula
[tex]v_{AE_{x}}=1.00\times10^{2}\cos24.5[/tex]
[tex]v_{AE_{x}}=0.90\times10^{2}\ mi/h[/tex]
For y axis,
[tex]v_{AE_{y}}=1.00\times10^{2}\sin24.5[/tex]
[tex]v_{AE_{y}}=0.41\times10^{2}\ mi/h[/tex]
Hence, (a). The components of the velocity of the jet airliner relative to the air is
[tex]v_{JA_{x}}=3.10\times10^{2}\ mi/h[/tex]
[tex]v_{JA_{y}}=0[/tex]
(b). The components of the velocity of the air relative to earth is
[tex]v_{AE_{x}}=0.90\times10^{2}\ mi/h[/tex]
[tex]v_{AE_{y}}=0.41\times10^{2}\ mi/h[/tex]