2D Compressor cascade study using DFLVR blade
i am analysing 2D compressor cascade using DFLVR blade, by varying its leading edge i am unable to find any standard test run of this blade,
if any one has done 2d-COMPRESSOR sTUDY THEN PLS HELP, i am facing a problem, in the result i am getting, i am using unstructured grid, inflow parameter as Pressure farfied(i am stimulating COmpressive flow at mach 1.4) and using a alue of 101325 pascal. and outflow as 1000pascal. i am using spalar allmaras scheme.
i am not getting good results. and also the grid is pretty schewed.
it would be great if i get some standard run case. which i can follow. its urgent.
i have to finish the work in 2 weeks
thanks in advance
Re: 2D Compressor cascade study using DFLVR blade
If you would like to send me the geometry, then I could prepare a ref. case for you.
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