The interaction between vortices, sound and combustion can lead to self-exc
ited oscillations of such large amplitudes that structural damage is done.
These occur because any small unsteadiness in the rate of combustion is a s
ource of sound, generating pressure and velocity fluctuations. However, the
velocity fluctuations perturb the flame, thereby altering the instantaneou
s rate of heat release. Instability is then possible because while acoustic
waves perturb the combustion, the unsteady combustion generates yet more s
ound! Combustion oscillations can occur in afterburners and at idle in conv
entional aeroengine combustors. Lean premixed, prevapourised technology has
tremendous potential to reduce NOx emissions, but is proving highly suscep
tible to self-excited oscillations. An overview of the physics of the inter
action between vortices, sound and flames is presented, and illustrated by
examples of instability in generic premixed ducted flames and in aeroengine
combustors. The potential for both passive and active control is discussed
.