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531
3
1 Geometry
1 Mesh
0 Simulation setups
0 ResultsCFD-Simulation of an internal geometry: A preliminary (2D) study of a turbulent, compressible flow (supersonic) in a Laval-Nozzle in a small Ejector operated with air at 300 K (inlet temperature). The pressure at inlet1 (bottom) is 5 bar (absolute). The flow through inlet2 (right side, normal pointing in x-direction) has an average speed of 0.1 m/s (inflow). The pressure at the outlet (top) is 1 bar (absolute). The geomertry is 2D (infinite in z-direction / no z-resolution). The boundary on the left is a symmetry plane. The other boundarys are walls (no-slip). The flow is to be modelled as turbulent (RANS).
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
by ahmedhussain18ahmedhussain18
ansheft created this project
over 9 years ago
1 Geometry 1 Mesh 0 Simulation setups 0 ResultsCFD-Simulation of an internal geometry: A preliminary (2D) study of a turbulent, compressible flow (supersonic) in a Laval-Nozzle in a small Ejector operated with air at 300 K (inlet temperature). The pressure at inlet1 (bottom) is 5 bar (absolute). The flow through inlet2 (right side, normal pointing in x-direction) has an average speed of 0.1 m/s (inflow). The pressure at the outlet (top) is 1 bar (absolute). The geomertry is 2D (infinite in z-direction / no z-resolution). The boundary on the left is a symmetry plane. The other boundarys are walls (no-slip). The flow is to be modelled as turbulent (RANS).
