| Item type |
紀要論文 / Departmental Bulletin Paper(1) |
| 公開日 |
2015-03-26 |
| タイトル |
|
|
タイトル |
A Preliminary Study of Supersonic Combustion in a Vitiated Airstream Using Transverse Injection |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
|
資源タイプ |
departmental bulletin paper |
| 著者 |
TSUJI, Hiroshi
TAKENO, Tadao
YOSHIDA, Akira
|
| 出版者 |
|
|
出版者 |
東京大学宇宙航空研究所 |
| 出版者（英） |
|
|
出版者 |
Institute of Space and Aeronautical Science,University of Tokyo |
| 書誌情報 |
en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo
巻 39,
号 7,
p. 143-159,
発行日 1974-03
|
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
An experimental investigation was conducted on the combustion of gaseous fuels injected normal to a supersonic airstream. City gas, ethylene and methane were injected transversely at sonic velocity from a circular injector in a flat plate (simulating the combustion chamber wall of a scramjet engine) into a Mach 1.10 vitiated airstream at an air total temperature of 1700°K and total pressure of about 2 atmospheres. Photographic observations of the flame shape were made to compare the edge of the luminous flame zone with the nonreacting jet penetration. The total pressure and the temperature surveys were made to examine the complex combustion flow field in the vertical and horizontal planes. As a result of the investigation, it was found that the edge of the luminous flame zone was correlated well with the nonreacting jet penetration. There was a relatively large recirculation region immediately downstream of the fuel jet, and the supersonic flow field with fuel injection was influenced only a little by the heat release. |
| ISSN |
|
|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0372-1418 |
| 書誌レコードID |
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|
収録物識別子タイプ |
NCID |
|
収録物識別子 |
AA00675986 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: SA2400963000 |
SA2400963.pdf (1.0 MB)
