In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and low....

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In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are \(70 m / s\) and \(63 m / s\) respectively. What is the lift on the wing if its area is \(2.5 m ^2\) ? The density of air is \(1.3 kg / m ^3\).  📲PW App Link - https://bit.ly/YTAI_PWAP 🌐PW Website - https://www.pw.live



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