The velocity at the outer edge of a two-dimensional incompressible boundary layer is defined by the...

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The velocity at the outer edge of a two-dimensional incompressible boundary layer is defined by the equation Ue =ax^1/2 (take a=2). In calculations, the case of suction and blowing from the wall will be considered and compared with solutions without blowing. The suction/blowing parameter will be taken as 0.3. After determining the differential equation to be solved and the boundary conditions, write code in a programming language of your choice for the solution. Use the Blasius method in solving the problem. The quantities to be obtained are as follows: a) Solve the equations and present your results in a table. b) Draw and compare the profiles of dimensionless velocity and shear stress. c) Find relationships for 8, 8*, and with the help of the solutions you found. Calculate the shape factor. The velocity at the outer edge of a two-dimensional incompressible boundary layer is defined by the equation Ue =ax^1/2 (take a=2). In calculations, the case of suction and blowing from the wall will be considered and compared with solutions without blowing. The suction/blowing parameter will be taken as 0.3. After determining the differential equation to be solved and the boundary conditions, write code in a programming language of your choice for the solution. Use the Blasius method in solving the problem. The quantities to be obtained are as follows: a) Solve the equations and present your results in a table. b) Draw and compare the profiles of dimensionless velocity and shear stress. c) Find relationships for 8, 8*, and with the help of the solutions you found. Calculate the shape factor.