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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![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.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F29446faa-3a85-4627-baa3-426fbb8bffe5%2F8a9a3080-3ecb-4ecd-9f8b-3e9e50099c70%2F3z6n21_processed.jpeg&w=3840&q=75)
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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