Acoustic-Structure Interaction: Modeling Sound Transmission Loss (STL) of a Finite Cylindrical Shell"

Please login with a confirmed email address before reporting spam

I everyone, ​I am trying to model the Sound Transmission Loss (STL) through a finite-length, thin-walled circular cylindrical shell in COMSOL Multiphysics and validate it against an analytical paper. ​Here are the specific details of the problem setup: ​Geometry & Physics: A finite-length isotropic cylindrical shell modeled using Love's thin shell theory. ​Acoustic Environment: The shell is excited from the outside by an oblique incident harmonic plane sound wave. The transmitted wave enters an interior anechoic cavity (non-reverberant / inward-traveling waves only). ​Boundary Conditions: The cylinder is Simply Supported (S-S) at both circular ends (v=0, w=0, N_{xx}=0, M_{xx}=0). ​I plan to use the Acoustic-Structure Interaction (Frequency Domain) interface with the Shell module for the structure and Pressure Acoustics for the fluid domains. ​Could anyone guide me on the best practices for setting up: ​The Background Pressure Field for an oblique incident plane wave acting on the outer cylindrical surface. ​The Perfectly Matched Layer (PML) or radiation boundary conditions inside the cylinder to properly simulate the anechoic core without artificial reflections. ​The exact constraints in the Shell interface to correctly replicate the Simply Supported conditions for a vibrating shell. ​Any model templates, expressions, or advice on capturing the stiffness, resonance, and mass-controlled regions accurately would be highly appreciated!

​Update on my current COMSOL setup and the issue I'm facing: ​To give more context, here is what I have already done in my model: ​Geometry: I have modeled a thin finite-length steel cylinder. Around this inner cylinder, I created a larger concentric cylinder domain to apply the Perfectly Matched Layer (PML). ​Material & Domains: Since both ends of the inner finite cylinder are open and the paper assumes air inside and outside, I have assigned Air to the entire domain inside the larger cylinder (which automatically covers both the exterior fluid and the fluid inside the open inner cylinder). ​Physics & Coupling: For the Acoustic-Structure Interaction, I have selected both the inner and outer curved surfaces of the steel cylinder. ​Loading & BCs: I implemented the Simply Supported boundary conditions on the shell edges. To simulate the external oblique plane wave, I applied a Boundary Load as a pressure distribution directly on the outer surface of the inner cylinder. ​The Issue: While the simulation runs and I am getting graphs, the results are not convincing and do not match the analytical curves from the paper. ​I suspect there might be an issue with: ​How I am applying the oblique plane wave as a manual Boundary Load instead of using COMSOL's built-in Background Pressure Field or Incident Acoustic Fields.

​Could anyone please point out the flaws in this approach or suggest how to correctly set up the incident plane wave and acoustic-structure coupling for this specific open-ended case?

please help me ,this is the paper link I am trying to get results in comsol

​Golzari, M., & Jafari, A. A. (2019). "Sound transmission through truncated conical shells." Applied Acoustics, 156, 186-207.



Reply

Please read the discussion forum rules before posting.

Please log in to post a reply.

Note that while COMSOL employees may participate in the discussion forum, COMSOL® software users who are on-subscription should submit their questions via the Support Center for a more comprehensive response from the Technical Support team.