CFD Analysis for flow between 2 compressor blades
Develop a CFD code that models the flow using the Euler equations. The code should use a finite volume method with Jameson’s scheme.
I computed the flow for three inlet Mach numbers: 0.3, 0.5 and 0.7 using for each case three grids: coarse, medium and fine. The grid size were following:
Coarse: 50x10
Medium: 100x20
Fine: 200x40
The code was solved using fortran and data analysis and plotting was done using MatLab
Flow analysis for Fine Grid: 200x40
Flow analysis for Fine Grid: 200x40
The flows for all the Mach Numbers are shown below, with a clear indication of a presence of shock wave when the flow velocity was near M=0.7
