jasonsum25
Subscriber
I am not sure the flow is supersonic in the inlet, should I input a value close to that of Total Gauge Pressure into Supersonic/Initial Gauge Pressure ? nI found online that Supersonic/Initial Gauge Pressure is predicted according to estimating the inlet velocity (incompressible) or the inlet Mach No. (compressible). If the case is super-sonic at inlet, this value must be specified. Otherwise, it'll be ignored by Fluent in subsonic case. nCan I type both Total Gauge Pressure and Supersonic/Initial Gauge Pressure with same /similar values in case I am not sure the flow is supersonic or subsonic?nThanks so much for answering!n
You are navigating away from the AIS Discovery experience