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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.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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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: 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/m² and the kinematic viscosity is 1.46*10³ m/s².
Transcribed Image Text: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: 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/m² and the kinematic viscosity is 1.46*10³ m/s².
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