1 research outputs found
An experimental investigation into the influence of installed chevron jet flows on wall-pressure fluctuations
Jet-surface interaction represents a significant community noise problem for the installation of
modern ultra-high bypass ratio turbofan engines. The use of chevron nozzles is known to reduce
low-frequency jet mixing noise by increasing the mixing rate close to the nozzle. It is currently
unknown, however, to what extent such a nozzle lip treatment affects the Kelvin-Helmholtz instability,
generated in the vicinity of the wing, which will modify the source of jet-surface interaction noise. To
clarify the physics of the jet-surface interaction noise source, an extensive experimental investigation
was conducted using the Flight Jet Rig in the anechoic chamber of the Doak Laboratory, at the
University of Southampton. Various measurements were carried out on a round and a chevron
single stream, unheated subsonic jet, both in an isolated configuration and installed beneath a 2D
NACA4415 airfoil "wing". The wall-pressure field on the wing surface was investigated using a pair
of miniature wall-pressure transducers and a set of ultra-thin precision microphones. These sensors
were flush-mounted in both the stream-wise and span-wise directions on the pressure side of the wing
and the unsteady wall-pressure data were analysed in the time and frequency domains. The far-field
noise results show significant broadband noise reduction by the chevron jet. This is further evidenced
by a reduction in the span-wise correlation length along the wing trailing edge over a wide range of
frequencies. Significant reduction of the tonal trapped wave energy is also observed