Although current theory for venturi scrubber efficiency assumes that gas-borne liquid flow rate, QL, remains constant throughout the scrubber, it actually varies as liquid evaporates, condenses, atomizes from the scrubber wall, or deposits to the wall. Experiments were conducted to measure QL at various locations in a venturi scrubber. Water was injected in two ways: (1) radially inward through a circumferential slot at the throat inlet, and (2) axially downward through a centered pipe at the converging section inlet. For each liquid injection arrangement, Q , was determined by measuring the water in the gas at 180 points in the venturi, under each of nine operating conditions defined by varying liquiddo-gas ratio and gas velocity in the throat. For radial injection, relatively little injected water was found to be gas borne throughou* the scrubber, whereas for axial injection, most or all injected water remained in the gas. For both liquid injection arrangements, the radial distribution of gas-borne liquid varied consistently with axial position; under every operating condition, the concentration of gas-borne liquid in the throat was highest near the injection point, whereas by the end of the diverging section, it was highest near the centerline. A mathematical model is proposed to explain the observed axial variations in gas-borne liquid Row rate.
NOMENCLATUREA total cross-sectional area, m2A, cross-sectional area tor location j, m2 C average droplet mass concentration 111 gas core, kg/m3 Koehler, Feldman, and Leith fractional penetration (fraction of particles of specified diameter not collected by scrubber), dimensionless gas volumetric flow rate, m3/s gas volumetric flow rate entering scrubber (measured), m3/s gas-borne liquid volumetric flow rate, m3/s liquid volumetric flow rate injected into scrubber (measured), m3/s injected liquid-to-gas ratio (measured), dimensionless liquid volumetric flow rate injected into scrubber (model input; see Table I), m3/s liquid volumetric flow rate on wall, m3/s instantaneous change in Q , at specified axial position, m3/s local scrubber radius, m inlet and outlet duct radi-US, m throat radius, m cross-sectional radius, m gas-phase Reynolds number, dimensionless wall surface area, m2 sum of squares droplet velocity relative to scrubber wall, m/s gas velocity relative to scrubber wall, m/s gas velocity in throat relative to scrubber wall, m/s ratio of actual liquid flow rate at location j to average liquid flow rate through scrubber cross section, dimensionless