• Scale effects in pantograph cavity coupling systems significantly influence aerodynamic noise generation, with smaller scales reducing overall radiated sound pressure levels.
• The dominant sound generation mechanism transitions from pure tone noise at larger scales to broadband noise at smaller scales due to turbulent boundary layer masking.
• A novel scale correction model combining sound source energy and dimensionless spectrum corrections enables accurate mapping of reduced-scale noise results to full-scale predictions.
• The findings provide critical insights for developing precision noise control technologies for high-speed trains.
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