Shock Loss Calculations Across Junctions and Splits.
Edwards JC; Perlee HE
NTIS#: PB 266 735 :9 pages
A computer code for laminar, steady-state, incompressible, two- dimensional flow, developed by gosman was modified by the Bureau of Mines to calculate shock (minor) loss at the intersections of ventilation ducts. Turbulent flow was simulated using laminar flow equations and an appropriate wall shear stress. Results of the calculation showed good agreement with the experiment.
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