Aviation Gas Turbine Combustion Test Rig
- 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