Figures & data
FIG. 1 Side-view schematic diagram of the experimental apparatus (not to scale). Straight duct sections are square in crosssection, 15 cm on a side by 152 cm long. The inset shows a close-up side view of an S-connector between two duct sections.
![FIG. 1 Side-view schematic diagram of the experimental apparatus (not to scale). Straight duct sections are square in crosssection, 15 cm on a side by 152 cm long. The inset shows a close-up side view of an S-connector between two duct sections.](/cms/asset/7b66e359-c9c7-4127-8a92-4d9a072c4f9c/uast_a_9705943_o_f0001g.gif)
FIG. 2 Dimensionless deposition velocities to S-connectors on the ceiling, wall, and floor at air speeds of (a) 2.2 m/s, (b) 5.3 m/s, and (c) 9.0 m/s.
![FIG. 2 Dimensionless deposition velocities to S-connectors on the ceiling, wall, and floor at air speeds of (a) 2.2 m/s, (b) 5.3 m/s, and (c) 9.0 m/s.](/cms/asset/86f725a0-231f-4f3c-a783-55a0384fcb1b/uast_a_9705943_o_f0002g.gif)
FIG. 3 S-connector deposition fraction versus connector Stokes number for S-connectors on the ceiling, wall, and floor at the three nominal air speeds.
![FIG. 3 S-connector deposition fraction versus connector Stokes number for S-connectors on the ceiling, wall, and floor at the three nominal air speeds.](/cms/asset/3653b229-fe68-4e36-99d9-91c8ac92d351/uast_a_9705943_o_f0003g.gif)
TABLE 1 Average S-connector deposition fractions in the bare steel duct systemFootnote a
FIG. 4 Penetration through (a) bend 5 and (b) bend 6 versus bend Stokes number for all air speeds in both the bare steel and insulated systems.
![FIG. 4 Penetration through (a) bend 5 and (b) bend 6 versus bend Stokes number for all air speeds in both the bare steel and insulated systems.](/cms/asset/de9a2655-a8a2-4777-9114-ed98e3839da7/uast_a_9705943_o_f0004g.gif)
FIG. 5 Composite dimensionless deposition velocities in (a) bend 5 and (b) bend 6 compared to dimensionless deposition velocities in straight steel ducts at nominal air speeds of 2.2 m/s, 5.3 m/s, and 9.0 m/s.
![FIG. 5 Composite dimensionless deposition velocities in (a) bend 5 and (b) bend 6 compared to dimensionless deposition velocities in straight steel ducts at nominal air speeds of 2.2 m/s, 5.3 m/s, and 9.0 m/s.](/cms/asset/f954e083-9be8-4b30-a348-bd26550c33f6/uast_a_9705943_o_f0005g.gif)
TABLE 2 Measured bend penetrations for all experimentsFootnote a
TABLE 3 Dimensionless deposition velocities for all panels in test duct 4 for all experimentsFootnote a Footnote b
FIG. 6 Enhancement factors at the ceiling, wall, and floor at panels in duct 4 in the bare steel system at three air speeds. Panels measure approximately 10 cm × 20 cm and are centered 30, 61, 91, and 122 cm downstream from the leading edge of a duct. See CitationSippola and Nazaroff (2004) for additional details.
![FIG. 6 Enhancement factors at the ceiling, wall, and floor at panels in duct 4 in the bare steel system at three air speeds. Panels measure approximately 10 cm × 20 cm and are centered 30, 61, 91, and 122 cm downstream from the leading edge of a duct. See CitationSippola and Nazaroff (2004) for additional details.](/cms/asset/a30bdfa5-3a89-4143-a4cd-6e66c5caeeff/uast_a_9705943_o_f0006g.gif)
FIG. 7 Enhancement factors at the ceiling, wall, and floor at panels in duct 4 in the insulated system at three air speeds. Panels measure approximately 10 cm × 20 cm and are centered 30, 61, 91, and 122 cm downstream from the leading edge of a duct. See CitationSippola and Nazaroff (2004) for additional details.
![FIG. 7 Enhancement factors at the ceiling, wall, and floor at panels in duct 4 in the insulated system at three air speeds. Panels measure approximately 10 cm × 20 cm and are centered 30, 61, 91, and 122 cm downstream from the leading edge of a duct. See CitationSippola and Nazaroff (2004) for additional details.](/cms/asset/1aabe510-c426-413a-b973-a4d1d7093f9d/uast_a_9705943_o_f0007g.gif)