Solution
Given angle "\\theta=72^0"
Speed of airliner
"V=\\sqrt{v_a^2+v_w^2+2v_av_w\\cos\\theta}"
Where "v_a, v_w" are speed of airliner and wind with respect to ground.
Therefore new speed of airliner ith respect to ground can be expressed as
"V=\\sqrt{(300)^2+(100)^2+2\\times (300)\\times (100)cos30^\u00b0}"
"V=389.82Km\/h"
Direction
"tan\\theta=\\frac{v_w}{v_a}=\\frac{100}{300}=0.33"
"\\theta= 18.26^\u00b0"
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