A pitot probe on an aircraft in a steady, level flight records a pressure of $55,000 \mathrm{~N} / \mathrm{m}^{2}$. The static pressure and density are $45,280 \mathrm{~N} / \mathrm{m}^{2}$ and $0.6 \mathrm{~kg} / \mathrm{m}^{3},$ respectively. The wing area and the lift coefficient are $16 \mathrm{~m}^{2}$ and 2 , respectively. The wing loading (in $\mathrm{N} / \mathrm{m}^{2}$ ) on this aircraft is____________ $\quad$ (accurate to one decimal place).

Question ID - 155537 :-

A pitot probe on an aircraft in a steady, level flight records a pressure of $55,000 \mathrm{~N} / \mathrm{m}^{2}$. The static pressure and density are $45,280 \mathrm{~N} / \mathrm{m}^{2}$ and $0.6 \mathrm{~kg} / \mathrm{m}^{3},$ respectively. The wing area and the lift coefficient are $16 \mathrm{~m}^{2}$ and 2 , respectively. The wing loading (in $\mathrm{N} / \mathrm{m}^{2}$ ) on this aircraft is____________ $\quad$ (accurate to one decimal place).

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