Calculation of the number of apertures in perforated sound-absorbing structures of an aircraft engine
A method for calculating the number of apertures in an aircraft engine’s perforated soundabsorbing structures that present themselves as shells of a rotating body with rectangular and circular guide is presented. Formulas for determining aperture pitch are given. Analytical expressions for calculati...
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Published in | Journal of machinery manufacture and reliability Vol. 44; no. 7; pp. 642 - 645 |
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Main Author | |
Format | Journal Article |
Language | English |
Published |
New York
Allerton Press
01.12.2015
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Subjects | |
Online Access | Get full text |
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Summary: | A method for calculating the number of apertures in an aircraft engine’s perforated soundabsorbing structures that present themselves as shells of a rotating body with rectangular and circular guide is presented. Formulas for determining aperture pitch are given. Analytical expressions for calculating the number of apertures in perforated areas with regular triangle and square lattices are presented. |
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ISSN: | 1052-6188 1934-9394 |
DOI: | 10.3103/S1052618815070158 |