i need the answer quickly Find the boundary layer thickness (8) equation, the shear stress (t.) and thecoefficient of drag (Cp) if the velocity distribution in the laminar boundary layer over theface of a spillway was observed to be:Then calculate the boundary layer thickness and drag force if the air flows over a sharpedged flat plate 0.25m long and 0.5m wide at a velocity 1 m/s, take the air density 1.23kg/m² and the kinematic viscosity is 1.46*10³ m/s².

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Find the boundary layer thickness (8) equation, the shear stress (t.) and the coefficient of drag (Cp) if the velocity distribution in the laminar boundary layer over the face of a spillway was observed to be: "1 U Then calculate the boundary layer thickness and drag force if the air flows over a sharp edged flat plate 0.25m long and 0.5m wide at a velocity 1 m/s, take the air density 1.23 kg/m³ and the kinematic viscosity is 1.46*10³ m/s².

Find the boundary layer thickness (8) equation, the shear stress (t.) and the coefficient of drag (Cp) if the velocity distribution in the laminar boundary layer over the face of a spillway was observed to be: "1 U Then calculate the boundary layer thickness and drag force if the air flows over a sharp edged flat plate 0.25m long and 0.5m wide at a velocity 1 m/s, take the air density 1.23 kg/m³ and the kinematic viscosity is 1.46*10³ m/s².

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter5: Analysis Of Convection Heat Transfer

Section: Chapter Questions

Problem 5.30P: Air at 1000C flows at an inlet velocity of 2 m/s between two parallel flat plates spaced 1 cm apart....

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