Q1: Find the boundary layer thickness (6) equation, the shear stress (to) and thecoefficient of drag (C₁) if the velocity distribution in the laminar boundary layer over theface of a spillway was observed to be:u7- (C)-()*+C)*.UThen 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/m³ and the kinematic viscosity is 1.46*10-5 m/s².

(a) To find: The expression for boundary layer thickness, the shear stress, and the coefficient of…

Q1: Find the boundary layer thickness (8) equation, the shear stress (to) 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: u y y “- ()--( ) + ( ). 2 3 +3 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 (Cp) if the velocity distribution in the laminar boundary layer over the face of a spillway was observed to be: u y y “- ()--( ) + ( ). 2 3 +3 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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