Q1: Find the boundary layer thickness (8) equation, the shear stress (to) and the coefficient of drag (Cò ) if the velocity distribution in the laminar boundary layer over the face of a spillway was observed to be: И 7- ()-()*+C). 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*105 m/s².
Q1: Find the boundary layer thickness (8) equation, the shear stress (to) and the coefficient of drag (Cò ) if the velocity distribution in the laminar boundary layer over the face of a spillway was observed to be: И 7- ()-()*+C). 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*105 m/s².
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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![Q1: Find the boundary layer thickness (6) equation, the shear stress (to) and the
coefficient of drag (Cò ) if the velocity distribution in the laminar boundary layer over the
face of a spillway was observed to be:
*--(C)- ()*+C).
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*10-5 m/s².](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F88723693-eae6-41f5-a6e2-a10850d68b58%2F3d38dd65-b6b9-4ec4-94d4-e4925f2bb296%2Fis3425c_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Q1: Find the boundary layer thickness (6) equation, the shear stress (to) and the
coefficient of drag (Cò ) if the velocity distribution in the laminar boundary layer over the
face of a spillway was observed to be:
*--(C)- ()*+C).
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*10-5 m/s².
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