Facilities
C. Kato Lab.
C. Kato Lab.

Pressure isosurfaces with velocity magnitude

This research aims to develop a numerical methodology for predicting aerodynamic noise generated by a propeller fan. To obtain validation data, we measured aerodynamic noise generated by a propeller fan. We are now performing numerical predictions based on large-scale LES of the broadband noise of a fan. The results to data seem to be quite promising.