Aerodynamic analysis of an aircraft fuselage
 

Hi,


I am currently performing a cfd simulation on openfoam to estimate the drag acting on the fuselage. The meshing of the fuselage is done on ansys meshing, cut-cell mesh with inflation is used and the y+ value is about 30, the turbulence model used is k-omega SST. On openfoam I am using the simplefoam solver.


Kindly help me with setting up the case especially the fvschems and fvsolution, the case file is uploaded kindly suggest me on the correct steps as I am trying such kind of simulation on Openfoam for the first time.


Thank you in advance.


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The initial conditions such as pressure and velocity are uploaded
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