Numerical prediction of aft radiation of turbofan tones through exhaust jets

Date

2009-08-07

Author

Özyörük, Yusuf

Metadata

Show full item record

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Item Usage Stats

14
views

0
downloads

Cite This

This paper describes a numerical methodology for calculating tonal noise propagation and radiation through turbomachinery exhaust ducts, including non-uniform background jet flows. The numerical method is based on solution of the linearized Euler equations directly in the frequency domain, employing a direct, sparse matrix solver in parallel. Acoustic sources are introduced into the computational domain via the perfectly matched layer equations. Various test cases including propagation through infinite ducts, and propagation and radiation through semi-infinite ducts with and without liners are solved, and results are compared with analytical solutions. It is demonstrated that solutions even with thin shear layers separating the exterior and jet streams at reasonably high Mach numbers can be obtained quite successfully. The method is also validated by simulating the radiated sound waves from two actual engine exhaust cowl geometries, and the results are compared with experimental data.

Subject Keywords

COMPUTATION, NOISE

URI

https://hdl.handle.net/11511/49276

Collections

Department of Aerospace Engineering, Article