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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 /

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. 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 \delta ,\delta *, and \theta 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???12(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. 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 ,**, and with the help of the solutions you found. Calculate
the shape factor.
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