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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Online Access: | https://www.mdpi.com/1996-1073/12/9/1746 |
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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 |
_version_ |
1725123195286061056 |