Axial compressor bleed modelling
Can anybody tell me how to modelling bleed massflow in a multistage axial flow compressor blade row using Ansys CFX.
The model is a mutli stage compressor with bleed in a rear stator blade row . There was no option to specify the bleed region using Turbogrid (pre processor) or model it in the CFX-pre.
I dont want to specify the entire shroud above the blade row as an outlet. I wanted to define a small area in the shroud as hole for bleed.
Did you find an answer for your question??
Actually I am trying to simulate the same problem that you mentioned here and I do not know how to do it.
It would be great if I can get some help,
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