shock systems in Laval nozzles with parallel side walls in detail by numerical and
experimental means. The location of the pseudo-shock system is defined in an adiabatic
system of two successive chocked Laval nozzles by the ratio of the critical cross sections
A2*/A1*, the stagnation pressure loss across the shock system and viscous losses.
Depending on the geometry and the test conditions, the pseudo-shock system attaches …