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The speed of air flow on the upper and lower surface of a wing of an aeroplane are v1 and v2 respectively if A is cross section area of the wing and rho is the density of air,then the upward lift is? (a)1/2 rho A(v2-v1) (b)1/2rho A(V1 V2) (C)1/2rho A(v1²-v2²) (d)1/2rho A(v1² v2²)? for NEET 2024 is part of NEET preparation. The Question and answers have been prepared
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The speed of air flow on the upper and lower surface of a wing of an aeroplane are v1 and v2 respectively if A is cross section area of the wing and rho is the density of air,then the upward lift is? (a)1/2 rho A(v2-v1) (b)1/2rho A(V1 V2) (C)1/2rho A(v1²-v2²) (d)1/2rho A(v1² v2²)?, a detailed solution for The speed of air flow on the upper and lower surface of a wing of an aeroplane are v1 and v2 respectively if A is cross section area of the wing and rho is the density of air,then the upward lift is? (a)1/2 rho A(v2-v1) (b)1/2rho A(V1 V2) (C)1/2rho A(v1²-v2²) (d)1/2rho A(v1² v2²)? has been provided alongside types of The speed of air flow on the upper and lower surface of a wing of an aeroplane are v1 and v2 respectively if A is cross section area of the wing and rho is the density of air,then the upward lift is? (a)1/2 rho A(v2-v1) (b)1/2rho A(V1 V2) (C)1/2rho A(v1²-v2²) (d)1/2rho A(v1² v2²)? theory, EduRev gives you an
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