What is it about?

The boundary layer on the surface of the fuselage plays a very important role on the resulting overall sound signature of an aeroplane during flight. The refraction and shielding produced by the presence of the fuselage boundary layer has been previously investigated using high-fidelity numerical methods. This work introduces an almost purely analytical approach to quantify the shielding and refraction effects of the boundary layer. That way, pressure in the near- and far-field can be calculated without th use of costly high-fidelity numerical schemes.

Featured Image

Read the Original

This page is a summary of: An Analytical Model of Sound Refraction By the Fuselage Boundary Layer for Fan Tone Radiation from a Turbofan Aero-engine, June 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2022-3059.
You can read the full text:

Read

Contributors

The following have contributed to this page