❌
d0=585vtσρl+597(μlσ⋅ρl)0.45(1000⋅QlQg)1.5d sub 0 equals the fraction with numerator 585 and denominator v sub t end-fraction the square root of the fraction with numerator sigma and denominator rho sub l end-fraction end-root plus 597 open paren the fraction with numerator mu sub l and denominator the square root of sigma center dot rho sub l end-root end-fraction close paren to the 0.45 power open paren 1000 center dot the fraction with numerator cap Q sub l and denominator cap Q sub g end-fraction close paren to the 1.5 power is in microns ( ), and velocities/properties are in metric units.
This document describes the objectives, inputs, methods, and worksheet structure for an upgraded Excel (XLS) tool to perform Venturi scrubber design calculations. It’s written to be directly usable as documentation and as a blueprint for implementing or updating an Excel workbook with calculation sheets, input validation, and reporting output. venturi scrubber design calculation xls upd
cause extreme structural erosion and excessive pressure drop without meaningful efficiency gains. Target a pressure drop budget between
: Determines the precise diameters and lengths for the converging , throat , and diverging sections based on target gas velocities. ❌ d0=585vtσρl+597(μlσ⋅ρl)0
): Often calculated using the Hesketh Equation , which factors in throat velocity, gas density, and liquid-to-gas (
Usually measured in Actual Cubic Feet per Minute (ACFM). cause extreme structural erosion and excessive pressure drop
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