Bernoulli's principle states that a wing with an area of 83 m² will experience a lift of 2767767.8 N when air moves over its top and bottom surface with velocities of aircraft 290 m/s and 180 m/s, respectively.
Bernoulli's principle is used to safely engineer the fluid flow within and around airplanes, engines and healthcare delivery devices by making sense of a fluid dynamics phenomenon. Bernoulli's principle connects a fluid's pressure to its speed.
The equation of Bernoulli's principle can be written as
P₁ + 1/2 p (v₁)² = P₂ + 1/2 p (v₂)²
P₁ - P₂ = 0.5* 1.29* 290² - 0.5* 1.29* 180² = 54244.5 - 20898 = 33,346.6
We know that, Pressure = Force/ Area
Force = Pressure * Area = 33,346.6* 83 = 2767767.8 N
Thus, the lift on the wing is 2767767.8 N.
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