Air of density 1.2 , kg , m^{-3} is blowing a | vedclass

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(C) According to Bernoulli's principle,for horizontal flow,the pressure difference $\Delta P$ is given by the equation:$\Delta P = P_{lower} - P_{uppe

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$7500$

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(C) According to Bernoulli's principle,for horizontal flow,the pressure difference $\Delta P$ is given by the equation:$\Delta P = P_{lower} - P_{upper} = \frac{1}{2} ho (v_{upper}^2 - v_{lower}^2)$Given:Density $ho = 1.2 \, kg \, m^{-3}$Velocity above the wing $v_{upper} = 150 \, m \, s^{-1}$Velocity below the wing $v_{lower} = 100 \, m \, s^{-1}$Substituting the values:$\Delta P = \frac{1}{2} 	imes 1.2 	imes (150^2 - 100^2)$$\Delta P = 0.6 	imes (22500 - 10000)$$\Delta P = 0.6 	imes 12500$$\Delta P = 7500 \, N \, m^{-2}$

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