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Shock Loss Calculations Across Junctions and Splits.
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.
IH; Report of Investigations
NTIS Accession No.
NTIS#: PB 266 735
Page last reviewed: April 12, 2019
Content source: National Institute for Occupational Safety and Health Education and Information Division