Tutorial Overview: Numerical Synergy in Muffler Acoustic Design A Critical Comparison of <scp>TMM</scp> , <scp>FEM</scp> , and <scp>CFD</scp> Approaches for Transmission Loss Quantification
ABSTRACT The acoustic optimization of mufflers in marine propulsion systems requires rigorous evaluation of transmission loss (TL) prediction methodologies, yet engineers often face challenges in selecting appropriate computational tools balancing accuracy and efficiency. This tutorial review provides a systematic comparison of three dominant approaches—Transfer Matrix Method (TMM), Finite Element Method (FEM), and Transient Computational Fluid Dynamics (CFD)—through the lens of both theoretical foundations and industrial applications. Beginning with didactic expositions of their mathematical formulations (plane wave theory, 3D Helmholtz solvers, and flow‐acoustic coupling), we establish standardized validation protocols using a canonical expansion chamber muffler case. Experimental measurements reveal distinct performance boundaries: TMM achieves rapid convergence (< 2 dB error below 2000 Hz) but neglects 3D wave effects; FEM maintains < 10% deviation up to 3500 Hz with 90% reduced computational cost versus CFD, while transient CFD captures broadband attenuation trends despite 10× higher resource demands. These findings deliver actionable workflows for muffler designers to strategically leverage TMM for conceptual screening, FEM for mid‐frequency optimization, and experimental‐correlated CFD for extreme flow conditions. The synthesis of theoretical rigor, numerical benchmarking, and marine‐specific implementation guidelines establishes this work as a foundational reference for both academic researchers and industrial practitioners in propulsion system acoustics.
Authors
- Xintie Wang
- Yi Yang
- Tong Wei
- Bin Fang
Institutions
- Marine Design & Research Institute of China (CN)
Publication Details
- Journal
- Engineering Reports
- Published
- 2025-12-23
- DOI
- https://doi.org/10.1002/eng2.70547
- Primary Topic
- Aerodynamics and Acoustics in Jet Flows
- Type
- article
- Field-Weighted Citation Impact
- 0.00