143146 An aeroplane of mass $3 \times 10^{4} \mathrm{~kg}$ and total wing area of $120 \mathrm{~m}^{2}$ is in level flight at some height. The difference in pressure between the upper and lower surface of its wings in kilopascal is $\left(\mathrm{g}=10 \mathrm{~m} / \mathrm{s}^{2}\right)$
143146 An aeroplane of mass $3 \times 10^{4} \mathrm{~kg}$ and total wing area of $120 \mathrm{~m}^{2}$ is in level flight at some height. The difference in pressure between the upper and lower surface of its wings in kilopascal is $\left(\mathrm{g}=10 \mathrm{~m} / \mathrm{s}^{2}\right)$
143146 An aeroplane of mass $3 \times 10^{4} \mathrm{~kg}$ and total wing area of $120 \mathrm{~m}^{2}$ is in level flight at some height. The difference in pressure between the upper and lower surface of its wings in kilopascal is $\left(\mathrm{g}=10 \mathrm{~m} / \mathrm{s}^{2}\right)$
143146 An aeroplane of mass $3 \times 10^{4} \mathrm{~kg}$ and total wing area of $120 \mathrm{~m}^{2}$ is in level flight at some height. The difference in pressure between the upper and lower surface of its wings in kilopascal is $\left(\mathrm{g}=10 \mathrm{~m} / \mathrm{s}^{2}\right)$