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-If the velocity distribution for the laminar boundary layer over a flat plate is given by :- U — هل 2 3 = 2₁ +2₂₂ x × ( 2 ) + 1 × ( 2 ) ² + 2 × ( Z ) ² Determine the form of the velocity profile by using the necessary boundary conditions. After that by using the Von- Karman integral momentum equation find an expression in terms of the Reynolds number to evaluate 1- Boundary Layer Thickness 2-Wall Shear Stress 3- Drag Force 4- Local and Average Skin Friction Coefficients 5- Displacement Thickness 6- Momentum Thickness 7- Energy Thickness

-If the velocity distribution for the laminar boundary layer over a flat plate is given by :- U — هل 2 3 = 2₁ +2₂₂ x × ( 2 ) + 1 × ( 2 ) ² + 2 × ( Z ) ² Determine the form of the velocity profile by using the necessary boundary conditions. After that by using the Von- Karman integral momentum equation find an expression in terms of the Reynolds number to evaluate 1- Boundary Layer Thickness 2-Wall Shear Stress 3- Drag Force 4- Local and Average Skin Friction Coefficients 5- Displacement Thickness 6- Momentum Thickness 7- Energy Thickness

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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-If the velocity distribution for the laminar boundary layer over a flat plate is given by :- 3 2 U x - 4 4 - (2) + 4 - (H) + 4 (2) + 22 X x U∞o Determine the form of the velocity profile by using the necessary boundary conditions. After that by using the Von- Karman integral momentum equation find an expression in terms of the Reynolds number to evaluate 1- Boundary Layer Thickness Force 4- Local and Average Skin Friction Coefficients 6- Momentum Thickness 7- Energy Thickness 2-Wall Shear Stress 3- Drag 5- Displacement Thickness
Transcribed Image Text:-If the velocity distribution for the laminar boundary layer over a flat plate is given by :- 3 2 U x - 4 4 - (2) + 4 - (H) + 4 (2) + 22 X x U∞o Determine the form of the velocity profile by using the necessary boundary conditions. After that by using the Von- Karman integral momentum equation find an expression in terms of the Reynolds number to evaluate 1- Boundary Layer Thickness Force 4- Local and Average Skin Friction Coefficients 6- Momentum Thickness 7- Energy Thickness 2-Wall Shear Stress 3- Drag 5- Displacement Thickness
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