Multistage orifice plates are widely used for pressure reduction and flow regulation, but conventional coaxial designs can lead to concentrated jets, local low-pressure regions, cavitation risk, and flow-induced noise. To improve throttling performance while reducing noise, a rotationally staggered multistage orifice plate is proposed, in which the holes in adjacent plates are circumferentially offset by a fixed angle. A numerical model based on the SST k – ω turbulence model is established and validated against experimental data, achieving a pressure drop error of less than 10%. The staggered arrangement is compared with conventional coaxial structures, demonstrating enhanced pressure-reduction capability and reduced low-pressure regions. An optimization framework combining Latin hypercube sampling, Spearman correlation analysis, surrogate modeling, and non-dominated sorting genetic algorithm II (NSGA-II) is developed. Compared with the original staggered structure, the optimized design maintains the required pressure drop, reduces the low-pressure magnitude by 12.0%, and decreases the maximum velocity by 3.37%. These results demonstrate the potential of the proposed design as a passive strategy for reducing noise in multistage throttling components.
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Jin et al. (2026) studied this question.
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