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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 twodimensional incompressible boundary layer is defined by the equation Ue axtake a In calculations, the case of suction and blowing from the wall will be considered and compared with solutions without blowing. The suctionblowing parameter will be taken as 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 twodimensional incompressible boundary layer is
defined by the equation Ue take In calculations, the case of suction and
blowing from the wall will be considered and compared with solutions without blowing.
The suctionblowing parameter will be taken as 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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