Effect of Combustor Configuration on Flow and Combustion in a Scramjet Engine
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Yang, Inyoung | ko |
| dc.contributor.author | Lee, Yang Ji | ko |
| dc.contributor.author | Lee, Kyung Jae | ko |
| dc.contributor.author | Park, Chul | ko |
| dc.date.accessioned | 2013-08-08T06:00:56Z | - |
| dc.date.available | 2013-08-08T06:00:56Z | - |
| dc.date.created | 2013-06-24 | - |
| dc.date.created | 2013-06-24 | - |
| dc.date.issued | 2013-05 | - |
| dc.identifier.citation | JOURNAL OF PROPULSION AND POWER, v.29, no.3, pp.751 - 756 | - |
| dc.identifier.issn | 0748-4658 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/174751 | - |
| dc.language | English | - |
| dc.publisher | AMER INST AERONAUTICS ASTRONAUTICS | - |
| dc.subject | SUPERSONIC-COMBUSTION | - |
| dc.subject | INLET | - |
| dc.title | Effect of Combustor Configuration on Flow and Combustion in a Scramjet Engine | - |
| dc.type | Article | - |
| dc.identifier.wosid | 000318826400027 | - |
| dc.identifier.scopusid | 2-s2.0-84878317989 | - |
| dc.type.rims | ART | - |
| dc.citation.volume | 29 | - |
| dc.citation.issue | 3 | - |
| dc.citation.beginningpage | 751 | - |
| dc.citation.endingpage | 756 | - |
| dc.citation.publicationname | JOURNAL OF PROPULSION AND POWER | - |
| dc.identifier.doi | 10.2514/1.B34737 | - |
| dc.contributor.nonIdAuthor | Yang, Inyoung | - |
| dc.contributor.nonIdAuthor | Lee, Yang Ji | - |
| dc.contributor.nonIdAuthor | Lee, Kyung Jae | - |
| dc.type.journalArticle | Article | - |
| dc.subject.keywordPlus | SUPERSONIC-COMBUSTION | - |
| dc.subject.keywordPlus | INLET | - |
- Appears in Collection
- Files in This Item
- There are no files associated with this item.
This item is cited by other documents in WoS
| ⊙ Detail Information in WoSⓡ | Click to see |  |
| ⊙ Cited 4 items in WoS | Click to see citing articles in |  |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.