need urgent help please!
hi, i am searching for a nozzle that has sharp Discontinuities in the profile. this sharp discontinuites disturb flow severly. i wat to calculate mach number effect from it and i want to ask that compressible solution is diverging. i am using coupled solver sith one equation model. i am using courant number 0.1. and pressure far field boundary condition at outlet.
|All times are GMT -4. The time now is 09:45.|