A strategy for optimizing the performance of a laboratory-scale combus
tor with respect to volumetric heat release (maximize) and pressure fl
uctuations (minimize) has been developed. This strategy utilized (1) a
ctuation techniques that simultaneously control volumetric heat releas
e and pressure fluctuations; (2) sensing techniques that measure combu
stor performance; and (3) an adaptive optimal control strategy. Actuat
ion techniques were chosen for their ability to alter the unsteady flo
w associated with the shear layer and recirculating flow regions of th
e combustor. Periodic spanwise forcing of the inlet boundary layer is
used to reduce combustion-induced pressure fluctuations. Crossflow jet
s upstream of the inlet are used to control volumetric heat release. S
ensing techniques were selected to measure or estimate the two perform
ance parameters to be controlled. A fast-response piezoelectric pressu
re transducer measure the magnitude of the pressure fluctuations. A st
reamwise array of photodiodes measures light emission from the flame a
nd enables estimation of volumetric heat release. Combustor performanc
e is explicitly defined in terms of a cost function that is a weighted
combination of rms pressure fluctuations and mean volumetric heat rel
ease. The control strategy performs an on-line minimization of the cos
t function by continuously seeking the optimal combination of actuator
settings and subsequently maintaining the cost at a minimum when the
combustor is subject to unknown inlet condition changes, such as flow
disturbances. The strategy has been tested with large flow disturbance
s and found capable of indirectly sensing a change in combustor inlet
conditions and finding the new optimal actuator settings.