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Parvin Mehr, Bradley M. Conrad, Matthew R. Johnson
Energy & Emissions Research Lab, Mechanical & Aerospace Engineering, Carleton University, Ottawa, Canada
Predicting Flare-Generated Black Carbon:
Progress Toward a Unified Model
for Aerodynamic and Fuel Chemistry Effects
Abstract
• Understanding the role of aerodynamic parameters and fuel chemistry effects on Black
carbon (BC) emissions is necessary for accurate models and emission factors
• Finding a suitable scaling parameter which correlates emissions to practical parameters in
the upstream oil and gas (O&G) industry is difficult and has been mostly restricted to
laminar flames and pure fuels.
Flaring Facility and BC Sampling System
Key conclusions• For turbulent flares, burning a range of alkane-based mixtures representative of flaring in
the upstream oil and gas industry, black carbon emissions correlate well with the carbon-
hydrogen ratio and fuel exit velocity
• Model works well for flares up to 2”, further lab and field experiments planned to push this
bounds
• Simple empirical correlation could be used to greatly improve inventory estimates
• Planned work will focus on extended test range, experiments in cross-wind conditions, and
more full-scale field measurements to test and validate and improve the presented model
OCECPASS3
Results
Comparison to literature
Cited publications[1] J.D.N.B. carbon particulate matter emission factors for buoyancy-driven associated gas flares McEwen, M.R. Johnson, Black carbon particulate
matter emission factors for buoyancy-driven associated gas flares, J. Air Waste Manag. Assoc. 62 (2012) 307–321.
doi:10.1080/10473289.2011.650040.
[2] M.A. Delichatsios, Transition from momentum to buoyancy-controlled turbulent jet diffusion flames and flame height relationships, Combust.
Flame. 92 (1993) 349–364. doi:10.1016/0010-2180(93)90148-V.
[3] H.A. Becker, D. Liang, Total emission of soot and thermal radiation by free turbulent diffusion flames, Combust. Flame. 44 (1982) 305–318.
doi:10.1016/0010-2180(82)90080-3.
•MFC
•MFC
•Filt.
•Filt.
•*
•*
Scaled with stack exit velocity as the
aerodynamic parameter
Scaled with higher heating value as the fuel
chemistry effect
Scaled with stack exit velocity as
the aerodynamic parameter and
higher heating value as the fuel
chemistry effect