In a modern turbo-fan engine, the afterburner flame-holders are positi
oned in the mixing flow between the core and bypass streams. These two
streams have different velocities and temperatures. They also have di
fferent duct lengths and, therefore, different acoustic properties. Th
e influence of such a twin-stream supply on acoustically coupled combu
stion oscillations is investigated in this paper. Measurements on an e
xperimental rig show how differences in the acoustic impedances, the m
ean velocities and the mean temperatures in the two supply streams lea
d to appreciably different unsteady heat release rates in the two stre
ams. These affect the frequency of the combustion oscillation. A theor
y explains these results and correctly describes the variation in freq
uency as the properties of the two supply streams are varied. (C) 1995
Academic Press Limited