Hot-jet ignition of a combustible mixture has application in IC engines, detonation initiation, and wave rotor combustion. Numerical predictions are made for ignition of combustible mixtures using a traversing jet of chemically active gas at one end of a long constant-volume combustor (CVC) with aspect ratio similar to a wave rotor channel. The CVC initially contains a stoichiometric mixture of ethylene or methane at atmospheric conditions. The traversing jet issues from a rotating pre-chamber that generates gaseous combustion products, assumed at chemical equilibrium for estimating major species. Turbulent combustion uses a hybrid eddy-break-up model with detailed finite-rate kinetics and a two-equation k-ω model. The confined jet is observed to behave initially as a wall jet and later as a wall-impinging jet. The jet evolution, vortex structure and mixing behavior are significantly different for traversing jets, stationary centered jets, and near-wall jets. Pressure waves in the CVC chamber affect ignition through flame vorticity generation and compression. The jet and ignition behavior are compared with high-speed video images from a prior experiment. Production of unstable intermediate species like C2H4 and CH3 appears to depend significantly on the initial jet location while relatively stable species like OH are less sensitive.
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ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
June 3–7, 2013
San Antonio, Texas, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5511-9
PROCEEDINGS PAPER
Traversing Hot-Jet Ignition in a Constant-Volume Combustor Available to Purchase
Abdullah Karimi,
Abdullah Karimi
Indiana University – Purdue University, Indianapolis, IN
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Manikanda Rajagopal,
Manikanda Rajagopal
Indiana University – Purdue University, Indianapolis, IN
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Razi Nalim
Razi Nalim
Indiana University – Purdue University, Indianapolis, IN
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Abdullah Karimi
Indiana University – Purdue University, Indianapolis, IN
Manikanda Rajagopal
Indiana University – Purdue University, Indianapolis, IN
Razi Nalim
Indiana University – Purdue University, Indianapolis, IN
Paper No:
GT2013-95797, V01BT04A059; 13 pages
Published Online:
November 14, 2013
Citation
Karimi, A, Rajagopal, M, & Nalim, R. "Traversing Hot-Jet Ignition in a Constant-Volume Combustor." Proceedings of the ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. Volume 1B: Combustion, Fuels and Emissions. San Antonio, Texas, USA. June 3–7, 2013. V01BT04A059. ASME. https://doi.org/10.1115/GT2013-95797
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