"\\overline{v}_{r}" − resulting velocity
"\\overline{v}_{a}" − aeroplane velocity
"\\overline{v}_{w}" − wind velocity
"v_{rx}", "v_{ax}", "v_{wx}" − x-components of the "\\overline{v}_{r}", "\\overline{v}_{a}" and "\\overline{v}_{w}", respectively
"v_{ry}", "v_{ay}", "v_{wy}" − y-components of the "\\overline{v}_{r}", "\\overline{v}_{a}" and "\\overline{v}_{w}", respectively
"\\lvert\\overline{v}_{r}\\rvert, \\lvert\\overline{v}_{a}\\rvert, \\lvert\\overline{v}_{w}\\rvert" − absolute values of resulting velocity, aeroplane velocity and wind velocity, respectively
1.
"\\overline{v}_{a}+\\overline{v}_{w}=\\overline{v}_{r}"
"v_{ax}-v_{wx}=0"
"\\lvert\\overline{v}_{a}\\rvert\\cdot\\sin\\beta-\\lvert\\overline{v}_{w}\\rvert\\cdot\\sin\\alpha=0"
"80\\cdot\\sin\\beta-30\\cdot\\frac{\\sqrt{2}}{2}=0"
"sin\\beta\\approx0.265"
"\\beta\\approx15.4^\\circ"
2.
"S=v\\cdot t=\\lvert\\overline{v}_{r}\\rvert\\cdot t"
"t=\\frac{S}{\\lvert\\overline{v}_{r}\\rvert}"
"\\lvert\\overline{v}_{r}\\rvert=\\sqrt{v_{rx}^2+v_{ry}^2}=\\sqrt{0+v_{ry}^2}=v_{ry}"
"v_{ay}-v_{wy}=v_{ry}"
"\\lvert\\overline{v}_{a}\\rvert\\cdot\\cos\\beta-\\lvert\\overline{v}_{w}\\rvert\\cdot\\cos\\alpha=v_{ry}"
"\\lvert\\overline{v}_{r}\\rvert=v_{ry}=80\\cdot0.964-30\\cdot\\frac{\\sqrt{2}}{2}\\approx55.9\\;m\/s"
"v[km\/h]=\\frac{v[m\/s]\\cdot1000}{3600}"
"\\lvert\\overline{v}_{r}\\rvert=\\frac{55.9\\cdot1000}{3600}\\approx15.5\\;km\/h"
"t=\\frac{200}{15.5}\\approx12.9\\;h"
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