The results of the investigation of the reactive flow in a scaled-down (con
gruent to 1:3) model of a gas turbine combustion chamber are presented. The
lean-premix combustion chamber model was tested at atmospheric pressure; m
easurements in the reactive flow were taken by using a two-channel fibre-op
tic laser Doppler anemometer with Al2O3 seeding on the air flow. Measuremen
ts cover a wide region of the axial-symmetric combustion chamber at points
characterised by different seeding conditions and data rates, including the
flame development and recirculating zones. This work presents a detailed a
nalysis of the fluctuating components of flow velocity; mean flow propertie
s are presented as a prerequisite. Frequency and time domain characteristic
s of turbulence including power density spectra, autocorrelation coefficien
ts and time integral scales are reported and discussed, and a physical desc
ription of the reacting turbulent flow field is attempted. (C) Elsevier, Pa
ris.