Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic Flow

This work focuses on forced combustion with regards to the relationship between vent mixer models and several injection locations in unheated supersonic flow. A plasma jet torch was used to ignite the hydrogen-air mixture in a laboratory-scaled combustor duct. The flow field of the combustion was vi...

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Main Authors: Chae-Hyoung Kim, In-Seuck Jeung
Format: Article
Language:English
Published: MDPI AG 2019-05-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/12/9/1746
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spelling doaj-2be67a02442a4756bc87690ed13ced762020-11-25T01:23:18ZengMDPI AGEnergies1996-10732019-05-01129174610.3390/en12091746en12091746Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic FlowChae-Hyoung Kim0In-Seuck Jeung1Engine Test and Evaluation Team, Korea Aerospace Research Institute, Daejeon 34133, KoreaDepartment of Mechanical and Aerospace Engineering, Seoul National University, Seoul 08826, KoreaThis work focuses on forced combustion with regards to the relationship between vent mixer models and several injection locations in unheated supersonic flow. A plasma jet torch was used to ignite the hydrogen-air mixture in a laboratory-scaled combustor duct. The flow field of the combustion was visualized with pressure and gas-sampling measurements. The vent mixers indicate good dispersion characteristics of the mixture for both parallel and normal 1 injections. However, forced combustion is dominantly governed by the injection rate toward the plasma jet (hot source) because the combustible region is restricted under the cold main flow. For this reason, the parallel injection, which provides the hydrogen-air mixture directly toward the plasma jet, shows good combustion performance. The normal 1 injection interacted with the vent mixers and shows slightly good combustion performance. Lastly, the normal 2 injection is little affected by the vent mixers and has poor combustion performance.https://www.mdpi.com/1996-1073/12/9/1746supersonic combustionvent mixermixingcombustion performance
collection DOAJ
language English
format Article
sources DOAJ
author Chae-Hyoung Kim
In-Seuck Jeung
spellingShingle Chae-Hyoung Kim
In-Seuck Jeung
Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic Flow
Energies
supersonic combustion
vent mixer
mixing
combustion performance
author_facet Chae-Hyoung Kim
In-Seuck Jeung
author_sort Chae-Hyoung Kim
title Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic Flow
title_short Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic Flow
title_full Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic Flow
title_fullStr Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic Flow
title_full_unstemmed Forced Combustion Characteristics Related to Different Injection Locations in Unheated Supersonic Flow
title_sort forced combustion characteristics related to different injection locations in unheated supersonic flow
publisher MDPI AG
series Energies
issn 1996-1073
publishDate 2019-05-01
description This work focuses on forced combustion with regards to the relationship between vent mixer models and several injection locations in unheated supersonic flow. A plasma jet torch was used to ignite the hydrogen-air mixture in a laboratory-scaled combustor duct. The flow field of the combustion was visualized with pressure and gas-sampling measurements. The vent mixers indicate good dispersion characteristics of the mixture for both parallel and normal 1 injections. However, forced combustion is dominantly governed by the injection rate toward the plasma jet (hot source) because the combustible region is restricted under the cold main flow. For this reason, the parallel injection, which provides the hydrogen-air mixture directly toward the plasma jet, shows good combustion performance. The normal 1 injection interacted with the vent mixers and shows slightly good combustion performance. Lastly, the normal 2 injection is little affected by the vent mixers and has poor combustion performance.
topic supersonic combustion
vent mixer
mixing
combustion performance
url https://www.mdpi.com/1996-1073/12/9/1746
work_keys_str_mv AT chaehyoungkim forcedcombustioncharacteristicsrelatedtodifferentinjectionlocationsinunheatedsupersonicflow
AT inseuckjeung forcedcombustioncharacteristicsrelatedtodifferentinjectionlocationsinunheatedsupersonicflow
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