This paper presents results from an investigation of the broadband sou
rces of acoustic noise in small axial flow fans. Observations drawn fr
om flow visualization experiments and fluid dynamic measurements indic
ate that secondary flows are primary contributors to the broadband noi
se generated by small axial flow fans. More specifically, how unsteadi
ness associated with tip gap flows is identified as a primary source o
f high frequency noise. As air is forced through the tip gap (i.e. the
space between the rotating blade tip and the stationary housing), the
flow rolls up forming vortices at the blade tip. These vortices conve
ct into the blade passage and become the dominant source of unsteadine
ss in the blade passage and at the fan exit plane. The data presented
indicates that this turbulence is the dominant source of noise above 1
.5 kHz for the fan tested. The likely radiation mechanisms are trailin
g edge scattering, and radiation from free turbulence and/or boundary
layers. Three types of experiments were performed as part of the study
. First, flow visualization tests were run in an attempt to obtain a s
ubjective evaluation of the flowfield. Then, stationary and rotating h
ot-wires were used to provide mean velocity and turbulence intensity d
ata for non-radial flow components. Using the results from the flow vi
sualization and hot-wire tests, possible noise generation mechanisms w
ere postulated. Fan modifications were then made to test the viability
of the proposed noise contributors. The addition of flanges to the bl
ade tips and of fabric near the blade trailing edges provided up to a
9 dB decrease in sound power above 1 kHz. These results will need to b
e coupled to an analogous study of low frequency noise generation (i.e
. below 1 kHz) for a significant reduction in perceived noise level to
be achieved. (C) 1998 Academic Press.