A solution will be sought for the velocity Ue = ax/2 at the outer edge of...

Transcribed Image Text:

A solution will be sought for the velocity Ue = ax/2 at the outer edge of a two-dimensional incompressible boundary layer (take a = 2). In the calculations, the case of wall suction/blowing will be considered, and the results will be compared with solutions without blowing. The suction/blowing parameter will be taken as 0.3. After defining the differential equation and boundary conditions to be solved, write code in the MATLAB programming language for the solution. The magnitudes to be obtained are as follows: a) Solve the differential equations by explaining them. Write the code that provides your results and present your results in a table. b) Find and explain the dimensionless velocity and shear stress equations. Through the code you wrote, draw and compare the profiles of dimensionless velocity and shear stress. c) With the solutions you have found, derive an expression for the boundary layer thickness (8), S* and momentum thickness (9). Calculate the shape factor. d) Interpret your results by comparing them. A solution will be sought for the velocity Ue = ax/2 at the outer edge of a two-dimensional incompressible boundary layer (take a = 2). In the calculations, the case of wall suction/blowing will be considered, and the results will be compared with solutions without blowing. The suction/blowing parameter will be taken as 0.3. After defining the differential equation and boundary conditions to be solved, write code in the MATLAB programming language for the solution. The magnitudes to be obtained are as follows: a) Solve the differential equations by explaining them. Write the code that provides your results and present your results in a table. b) Find and explain the dimensionless velocity and shear stress equations. Through the code you wrote, draw and compare the profiles of dimensionless velocity and shear stress. c) With the solutions you have found, derive an expression for the boundary layer thickness (8), S* and momentum thickness (9). Calculate the shape factor. d) Interpret your results by comparing them.