Facilities

FACILITIES

 

GAS TURBINE COMBUSTION LABORATORY

 

Two full-scale, gas-turbine spray-combustion models with high pressure and flow capabilities is available in this laboratory. The combustors can operate with a variety of liquid or gaseous fuels and are designed to allow active (acoustic) and passive forcing of the nozzle flows, and the use of nonintrusive flow and combustion diagnostics. State-of-the-art Planar Laser Induced Fluorescence (PLIF), Phase Doppler Velocimetry and Particle Size Analysis (PDV & PSA), Rainbow Thermometry and Stereoscopic Digital Particle Image Velocimetry (SDPIV) systems are installed. A smaller scale model gas turbine combustor is available for atmospheric pressure tests.

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Spray Combustor

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Trapped Vortex Combustor

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Fuel injector spray measurements.