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Sökning: L773:1270 9638 > (2020-2024) > Large Eddy Simulati...

LIBRIS Formathandbok  (Information om MARC21)
FältnamnIndikatorerMetadata
00003948naa a2200337 4500
001oai:lup.lub.lu.se:70166d97-a833-4848-8a3a-e43935cf8e96
003SwePub
008231024s2023 | |||||||||||000 ||eng|
024a https://lup.lub.lu.se/record/70166d97-a833-4848-8a3a-e43935cf8e962 URI
024a https://doi.org/10.1016/j.ast.2023.1085032 DOI
040 a (SwePub)lu
041 a engb eng
042 9 SwePub
072 7a art2 swepub-publicationtype
072 7a ref2 swepub-contenttype
100a Fureby, Christeru Lund University,Lunds universitet,Värmeöverföring,Institutionen för energivetenskaper,Institutioner vid LTH,Lunds Tekniska Högskola,LTH profilområde: Energiomställningen,LTH profilområden,Heat Transfer,Department of Energy Sciences,Departments at LTH,Faculty of Engineering, LTH,LTH Profile Area: The Energy Transition,LTH Profile areas,Faculty of Engineering, LTH4 aut0 (Swepub:lu)ch1708fu
2451 0a Large Eddy Simulation of cavity stabilized ramjet combustion
264 1c 2023
520 a In this study we use finite rate chemistry Large Eddy Simulation (LES) to examine flow, injection, mixing, self-ignition and turbulent combustion in a dual-mode ramjet combustor with a cavity flameholder. The target case is the dual-mode ramjet combustor studied experimentally by Micka & Driscoll in a series of publications under different operating conditions characterized by varying air stagnation temperatures, T0, and fueled with hydrogen or hydrogen-ethylene blends. Here, only hydrogen fuel is considered. Three skeletal and comprehensive chemical reaction mechanisms are used to evaluate the influence of the reaction mechanism. Based on comparisons with ignition, laminar flame, and dual-mode ramjet combustor experiments the Z22 mechanism is found superior to the D7 and J20 mechanisms, which is then used throughout this study. For the ramjet experiments, two stabilization modes were reported: cavity-stabilized combustion at low T0 and jet-wake-stabilized combustion at high T0. For in-between values of T0, combustion oscillates between these modes. The LES results using the Z22 reaction mechanism are in good agreement with the experimental data: cavity-stabilized combustion is observed for low T0, and for this case combustion anchors at the leading-edge of the cavity. For high T0 jet-wake-stabilized combustion occurs in the near-wake of the fuel-plume. Between these two modes, combustion oscillates between modes that can be roughly identified as jet-wake and cavity stabilized. The LES predictions also reveal details about high-frequency oscillations (∼1 kHz) that are observed in particular for low and intermediate T0. The H2-air mixture appears to burn as an auto-ignition assisted premixed flame in the cavity-stabilized case, and as a diffusion-flame in the jet-wake stabilized case, whereas for the in-between cases, the burning modes changes accordingly.
650 7a TEKNIK OCH TEKNOLOGIERx Maskinteknikx Strömningsmekanik och akustik0 (SwePub)203062 hsv//swe
650 7a ENGINEERING AND TECHNOLOGYx Mechanical Engineeringx Fluid Mechanics and Acoustics0 (SwePub)203062 hsv//eng
653 a Cavity stabilized ramjet combustion
653 a Combustion modes
653 a LES
653 a Unsteady supersonic combustion
700a Nilsson, Thommieu Lund University,Lunds universitet,Värmeöverföring,Institutionen för energivetenskaper,Institutioner vid LTH,Lunds Tekniska Högskola,Heat Transfer,Department of Energy Sciences,Departments at LTH,Faculty of Engineering, LTH4 aut0 (Swepub:lu)ener-ten
710a Värmeöverföringb Institutionen för energivetenskaper4 org
773t Aerospace Science and Technologyg 141q 141x 1270-9638
856u http://dx.doi.org/10.1016/j.ast.2023.108503x freey FULLTEXT
8564 8u https://lup.lub.lu.se/record/70166d97-a833-4848-8a3a-e43935cf8e96
8564 8u https://doi.org/10.1016/j.ast.2023.108503

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Fureby, Christer
Nilsson, Thommie
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TEKNIK OCH TEKNOLOGIER
TEKNIK OCH TEKNO ...
och Maskinteknik
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Lunds universitet

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