Research Article | OPEN ACCESS
Experiment and CFD Analysis of Reactive Muffler
1Yunshi Yao, 2Shaodong Wei, 1Jinpeng Zhao, 1Shibin Chen, 1Zhongxu Feng and 3Jinxi Yue
1Key Laboratory for Highway Construction Technology and Equipment of Ministry of Education, Chang
Research Journal of Applied Sciences, Engineering and Technology 2013 17:3282-3288
Received: January 18, 2013 | Accepted: March 02, 2013 | Published: September 20, 2013
Abstract
A conventional muffler used in vibratory rollers is usually designed based on experience and its performance could be enhanced in a large degree through structure optimization. In order to evaluate performance of reactive muffler and its effect on power loss of engine, flow field of muffler was discussed by CFD comparing with experimental test and the structure of reactive muffler was optimized. Based on results of simulation and optimization, the reactive muffler used in vibratory rollers with weight of 13t was fabricated and its field test was carried on. The simulate results showed that velocity field coincided with the pressure field basically, which indicates that the optimized muffler -2# has excellent aerodynamic characteristics and rational design of damping units. The results of field tests showed that 2# muffler had better acoustic insertion loss with little pressure loss. Acoustic insertion loss was 17~18.4 dB (A) at engine speed of 2450 rpm, which meets the designing goal.
Keywords:
Acoustic insertion loss, computational fluid dynamics, flow field, pressure loss, reactive muffler,
Competing interests
The authors have no competing interests.
Open Access Policy
This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.
Copyright
The authors have no competing interests.
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ISSN (Online): 2040-7467
ISSN (Print): 2040-7459 |
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