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Combustion Research Center (CRC)

MISSION

CRC supports industrial research and development of advance state-of-the-art
gas turbine combustor technologies to reduce fuel consumption by 60%, and
LTO and cruise NOx emission by 80% relative to CAEP 6 by 2025

CLIENTS

GE Aviation, GE Power and Water, GE GRC, Parker and Hannifin, SVT, NASA

RESEARCH

  • Turbulent Combustion
  • Novel Injectors
  • Development Spray Analysis
  • Low NOx Combustor Technologies (LDI, DLN)
  • Combustion Dynamics
  • Non-intrusive Diagnostics

FACILITIES

    • High Altitude Relight Test Facility
    • High Pressure Test Rig #1
    • High Pressure Test Rig #2
    • High Pressure Test Rig #3
    • Horizontal Test Rigs
    • Vertical Test Stands
    • Spray Test Facility
    • Water Tunnel #1

Spray Characterization

  • 2 x PDPA Systems
  • 1 x Spray Patternator
  • 2 x Particle Analyzers

Fuel-Air Mixing Characteristics

  • 1 x PLIF system
  • 1 x In-house Gas Sampling system

Combustor Aerodynamics

  • LDA systems
  • 1 x high-speed PIV system (10 KHz)
  • 1 x Standard PIV system

Combustion Diagnostics

  • 1 x PLIF system
  • 1 x high-speed IR camera
  • Time-Resolved Spectroscopy
  • Temperature and major species

Emission Analysis

  • HC, O2, NOx, CO
  • FTIR Analyzer
  • Laser-Induced Breakdown Spectroscopy

Miscellaneous Equipment

  • 3 x high-speed Cameras up to 100 fps
  • Several DAQ systems
  • Several 3D Traverses
  • Argon Ion, Nd-YAG and Dye Lasers



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College of Engineering & Applied Science | Department of Aerospace Engineering & Engineering Mechanics