Consider an airplane flying with a velocity of 60 m/s at a standard sea level conditions. At a point on the wing, the airflow velocity is 70 m/s. Calculate the pressure at this point. Assume incompressible flow. *Include the units on the answer.
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The Bernoulli's principle equation is: \[ P_1 + \frac{1}{2} \rho V_1^2 = P_2 + \frac{1}{2} \rho V_2^2 \] where: \( P_1 = 1 \text{ atm} = 1 \times 10^5 \text{ Pa} \) (standard sea level pressure) \( V_1 = 60 \text{ m/s} \) (airplane velocity) \( V_2 = 70 \text{ Show more…
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