Explanations & Calculations
- The length of the control wire should be 8m not 8cm
- "\\small \\omega=\\small0.25rps =\\small2\\pi\\times 0.25 rads^{-1}"
- Horizontal component of the tension provides the centripetal force needed to move in the circle while vertical component balances the weight of the aircraft to keep it horizontal
Therefore, applying Newton's second law towards the center of the circular path,
"\\qquad\\qquad\n\\begin{aligned}\n\\small T\\cos30 &= \\small mr\\omega^2=m(L\\cos 30)\\omega^2 \\\\\n\\small T &= \\small mL\\omega^2 \\\\\n&=\\small0.4kg\\times 8m\\times (2\\pi\\times 0.25)^2\\\\\n&= \\small \\bold{7.896\\,N}\n\\end{aligned}"
- T can be calculated considering the vertical equilibrium also but as the g is approximated to be 10ms-2 it gives T's value as 8N. If g is taken as 9.8ms-2 T gets the normal value as calculated above.
2, The lift on the plane = "\\small T\\sin 30=7.896\\times 0.5= 3.948\\,N"
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