TY - GEN
T1 - Effect of impingement angle on flame stability in a non-premixed methane/oxygen diffusion flame burner
AU - Ianuzzi, Makayla L.L.
AU - Hollingshead, Joshua M.
AU - Moore, Jeffrey D.
AU - Risha, Grant A.
N1 - Funding Information:
The authors wish to thank the Penn State Altoona Research and Sponsored Programs Office and Mr. Corey Griffin for sponsoring this internally-funded effort. Special thanks to Mr. Tom Hatch, Mr. Russ Heaton, and Mr. Jonathan Hileman for fabrication of the impingement angle injector end caps.
Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2020
Y1 - 2020
N2 - The focus of this research work was understanding the effect of varying the impingement angle of a single coaxial injector in an experimental non-premixed flame burner on flame stability. The reactants were methane and oxygen, mixed and ignited in a horizontally-mounted, rectangular combustion chamber using a retractable spark plug. Gaseous oxygen was the primary flow and gaseous methane was the secondary flow. Three injectors were fabricated with exit impingement angles of 15o, 30o, and 45o with the primary flow. Using optical windows on both sides of the chamber parallel to the axis of the flame, the product flame behavior and flame standoff distance was observed. Stability maps of the non-premixed flame behavior based upon equivalence ratio, reactant Reynolds numbers, and injector impingement angle were created. It was observed that the 15o impingement angle injector generated the most stable, anchored diffusion flames for high equivalence ratios and low Reynolds numbers. As impingement angle increased, stable, anchored flames transitioned from existing at fuel-lean highly turbulent primary flows to fuel-rich, highly turbulent flows as well as from fuel-rich, low primary flows to no ignition under the same conditions. Therefore, secondary flow impingement angle can drastically influence the location and range of stable, anchored GCH4/GO2 diffusion flames.
AB - The focus of this research work was understanding the effect of varying the impingement angle of a single coaxial injector in an experimental non-premixed flame burner on flame stability. The reactants were methane and oxygen, mixed and ignited in a horizontally-mounted, rectangular combustion chamber using a retractable spark plug. Gaseous oxygen was the primary flow and gaseous methane was the secondary flow. Three injectors were fabricated with exit impingement angles of 15o, 30o, and 45o with the primary flow. Using optical windows on both sides of the chamber parallel to the axis of the flame, the product flame behavior and flame standoff distance was observed. Stability maps of the non-premixed flame behavior based upon equivalence ratio, reactant Reynolds numbers, and injector impingement angle were created. It was observed that the 15o impingement angle injector generated the most stable, anchored diffusion flames for high equivalence ratios and low Reynolds numbers. As impingement angle increased, stable, anchored flames transitioned from existing at fuel-lean highly turbulent primary flows to fuel-rich, highly turbulent flows as well as from fuel-rich, low primary flows to no ignition under the same conditions. Therefore, secondary flow impingement angle can drastically influence the location and range of stable, anchored GCH4/GO2 diffusion flames.
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U2 - 10.2514/6.2020-3921
DO - 10.2514/6.2020-3921
M3 - Conference contribution
AN - SCOPUS:85091312749
SN - 9781624106026
T3 - AIAA Propulsion and Energy 2020 Forum
SP - 1
EP - 8
BT - AIAA Propulsion and Energy 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Propulsion and Energy 2020 Forum
Y2 - 24 August 2020 through 28 August 2020
ER -