March 8, 2021 at 6:18 pm
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Hello,nAbout the details of the mesh : 0.71 million elements, 0.4 million nodes, Triangles except for inflationn
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nAspect Ratio : (moyenne = average)n
nSkewness :n
nOrthogonal Quality :n
nHere are the Mesh quality given by Fluent : n
nThese are the General options :n
nA clarification concerning the boundary conditions, I used a 'Pressure-Inlet' condition for the 'Outlet 1' and a 'Pressure outlet' condition for 'Outlet'. To be noted, I used the identical backflow Turbulent length scale for every boundary condition. (0.006m : diameter of the nozzle exit). This might be something to be improve. Regarding the Thermal component, I used for every boundary condition 300K. n
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nAbout the Solution Methods you asked :n
nAbout the Solution Controls choices. I can not increase or decrease the Courant Number with this set-up (Density-based + Steady). During my simulation, I decreased them until 0.1.n
nI used a hybrid-initilization. I did not use the command /solve/initialize/fmg yes. This could be helping. n
nAbout the Free Courses, I found this one :n
and this one : n
But you are probably talking about this one ?n
nNone of them are dealing with a Supersonic Impinging jet but I will work on it!nnThank you for your help!nnGuillaumen















