In the field of aeronautics and astronautics, it is not convenient to directly arrange the conventional uniform distribution micro perforated panels on the structural parts in the noise reduction design of some structural components.However, there is few study on the sound absorption mechanism of unconventional arrangement micro perforated panels.Therefore, a segmented end correction method based on Fok function was proposed to analyse the unconventional micropore arrangement of annular micro perforated panels.The velocity distribution of the air particles near the micropore was analyzed by means of simulation.On this basis, the end correction was improved.A sample was made and tested in an impedance tube system, and the results were compared with those of the theoretical calculation.It is shown both are in good agreement.Moreover, both the experimental and theoretical results demonstrate that the trend of the absorption peak frequency of the unconventional micro perforated panel with annular arrangement is the same as that of the conventional.Based on the theory of segmented end modification, the method can be used not only in the structural design of unconventional micro perforated panels, but also in the back analysis of irregular micro perforated panels by measuring the sound absorption performance of the structure.
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