Let air at rest at the front edge of wing of an aeroplane and air passing over the surface of the wing at a fast speed `v`. If density of air is `rho`, then find out the highest value for `v` in stream line flow when atmospheric pressure is `P_(atm)`.

Let air at rest at the front edge of wing of an aeroplane and air pass

1.	Let air at rest at the front edge of wing of an aeroplane and air passing over the surface of the wing at a fast speed `v`. If density of air is `rho`, then find out the highest value for `v` in stream line flow when atmospheric pressure is `P_(atm)`.
Answer» Correct Answer - `v_(max) = ((2p_(atm))/(P))^(1//2)`

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Let air at rest at the front edge of wing of an aeroplane and air passing over the surface of the wing at a fast speed `v`. If density of air is `rho`, then find out the highest value for `v` in stream line flow when atmospheric pressure is `P_(atm)`.

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