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0 ResultsTo analysis the flow of air in a convergent-divergent nozzle, with the inlet Mach number as 0.5
by slilbaekslilbaek
jagatheaswaran created this project
about 5 years ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsTo analysis the flow of air in a convergent-divergent nozzle, with the inlet Mach number as 0.5
