The air density fluctuations in the plumes of fully expanded, unheated free jets were
investigated experimentally using a Rayleigh-scattering-based technique. The point
measuring technique used a continuous-wave laser, fibre-optic transmission and photon counting electronics.
The radial and centreline profiles of time-averaged density
and root-mean-square density fluctuation provided a comparative description of jet
growth. To measure density fluctuation spectra a two-photomultiplier-tube (PMT)
technique was used. Cross-correlation between the two PMT signals significantly
reduced the electronic shot noise contribution. The density fluctuation spectra were
found to be remarkably similar for all Mach number jets. A detailed survey in fully
expanded Mach 0.95, 1.4 and 1.8 jets further confirmed that the distribution of various
Strouhal frequency fluctuations remained similar, except for a spatial stretching
with increased Mach number. In spite of this similarity in flow fluctuations the noise
sources in these three jets were found to be significantly different. Spark schlieren
photographs and near-field microphone measurements confirmed that Mach wave
radiation was present in the Mach 1.8 jet, and was absent in the Mach 0.95 jet. Direct
correlation measurement between the flow density fluctuation (cause) and far-field
sound pressure fluctuation (effect) shed further light on the sound generation process.
For this purpose a microphone was kept fixed at a far-field point, mostly at a distance
of 50 diameters and 30° to the flow direction, and the laser probe volume was moved
from point to point in the flow. In the Mach 1.8 jet, where the convective velocity
of Kelvin–Helmholtz instability waves exceeded the ambient sound speed, significant
correlation was measured from the peripheral shear layer, while in the Mach 0.95
jet, where the instability waves had subsonic convective speed, no correlation could
be measured. Although the same instability waves were present in both Mach 1.8
and 0.95 jets, the peripheral shear layer of the former was found to be an obvious
noise source, while that of the latter was not. Further correlation studies along the
jet centreline showed that behaviour in the region downstream of the potential core
was similar in all Mach number jets tested, 0:6[les ]M[les ]1:8. Good correlation at low
Strouhal frequencies was measured from this region, which started from downstream
of the potential core and extended many diameters from there.