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QJEEM24Phed9c: JEE Main 2024 Physics - Class 11 JEEM24Phed9c Solution: In a test experiment on a model aeroplane in wind tunnel, the…

In a test experiment on a model aeroplane in wind tunnel, the flow speeds on the upper and lower surfaces of the wings are 70 ms−1 and 65 ms−1 respectively. If the wing area is 2 m2, the lift of the wing is _________ N.

(Given density of air =1.2 kg m−3)

Step-by-Step Verified Solution

F=12ρ(v12−v22)AF=12×1.2×(702−652)×2=810 N

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