Evaluate the displacement thickness δ* and the momentum thickness θ for a power law velocity profile given by
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- a. If the velocity distribution for the laminar boundary layer over a flat plate is given by :- ** (²) ² - 21 + A₂ x U A₁ + A₂ x 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 2-Wall Shear Stress 3-Drag 5- Displacement Thickness + A₁ x 4- Local and Average Skin Friction Coefficients 6- Momentum Thickness 7- Energy Thicknessarrow_forwardConsider how the new geometry in this problem affects the math/boundary condition/derivation. Both equations are listed!arrow_forwardDetailed Solutionarrow_forward
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