All Stories

  1. Effective density and volatility of particles sampled from a helicopter gas turbine engine
  2. Particle Emission Characteristics of a Gas Turbine with a Double Annular Combustor
  3. Integrating Hypersonics into a Combustion Test Facility with 3D Viewing Capability
  4. Methane-Oxygen Flame Stability in a Generic Premixed Gas Turbine Swirl Combustor at Varying Thermal Power and Pressure
  5. Effective Density and Mass-Mobility Exponent of Aircraft Turbine Particulate Matter
  6. Differential Mobility Spectrometer Particle Emission Analysis for Multiple Aviation Gas Turbine Engine Exhausts at High and Low Power Conditions and a Simulated Gas Turbine Engine Exhaust
  7. The effect of variable fuel composition on a swirl-stabilised producer gas combustor
  8. Evaluation of Transport Line Effects on PM Size Distribution for Aircraft Exhaust for Different Flow Regimes and Dilution Methodology
  9. Evaluation of Methods for Measuring Particulate Matter Emissions from Gas Turbines
  10. Evaluation of a Particulate Sampling Methodology From a Gas Turbine Exhaust Using Real-Time Size and Number Analysis at Simulated Aircraft Conditions
  11. Mass and Size Distribution Measurements of Particulates from a Gas Turbine Combustor Using Modern Mobility Analyzer and Particle Sizer
  12. Detailed Internal Measurements of a Siemens Combustor Operating at Gas Turbine Relevant Conditions