Can some help me about designing 3D axial compressor?
I am an University student major in propulsion. Now I have to design a multistage axial compressor for my assignment, at least one stage. And I have the
radical distributions of the stator &rotor geometry parameters downloaded from NASA. But I am at sea about how to continue,like using which design codes.
Can anybody so kind to give me some advice?
Thank you in advance!
Try to read the documentation about turbomachinery course developed by ansys. You can easily to find it on the internet.
When you read this documents, try to come here with more specific doubts, because you have a lot to things to do...
|All times are GMT -4. The time now is 09:25.|