Abstract
The analysis of known calculated dependences for determining the relative cut-in length of the end hole of the channel
 without clamping shoulder (end correction) needed to perform applicative acoustic calculation, in particular by the design
 of jet noise mufflers. The accuracy of the results obtained by calculating with the known dependencies is estimated.
 The method of calculating of the end correction with machine method is offered, the basis of which was used by the
 development of analytical dependence for calculating the values of the cut-in length of the holes without clamping shoulder
 with high accuracy adopted in this article as a reference. These values are calculated in Matlab system with relative and
 absolute accuracy 10–7 and 10–12, in particular, it was found that when ka=0l/a=0,6127, but not 0.6133 as it was previously
 thought in the world acoustics. A computer approach of calculation of the modified Bessel functions for large values of the
 argument was developed. A correction of design equations which are widely used in acoustic engineering development,
 which increases the accuracy of calculating the cut-in length of the end channels holes without clamping shoulder. The
 results are intended for use in both basic acoustic investigations and in their numerous practical applications.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.