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

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Дата загрузки:
06.07.2024 04:01
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00:03:15
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Обучение

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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 2m2 the lift of the wing is 810 N. (Given density of air = 1.2 kgm−3) JEE Main 2024

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