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I have a project on finite elements and want to explore this type of nozzles in Multiphysics simulation showing the shock waves that occur and the critical speeds, and calculated using a rate that can be seen in the attachment. I have a breakthrough that enclose
Please I need someone who can help me, the design of the nozzle has a perfect design and was tested physically
ASIM/MP does not support supersonic compressible flow which shock waves occurs, what is the Ma number in the nozzle?
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