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Aviation Gas Turbine Combustion Test Rig

Gas Turbine

  • Design Characteristics
    • Square 106 mm x 106 mm Cross-Section
    • Four-Sided Optical Access for Simultaneous PIV/PLIF, stereo PIV demonstrated recently
    • Water-Cooled Hardware
    • Low Frequency and High-Frequency Instrumentation
    • Laser Ignition
  • Demonstrated Steady-State Conditions
    • 1.5 MW thermal power
    • 2.14 MPa P3.1
    • 760 K T3.1
  • Over 150 hours of hot-fire time
  • Part of ZL3 Lab