| アイテムタイプ |
itemtype_ver1(1) |
| 公開日 |
2024-10-21 |
| タイトル |
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|
タイトル |
Synchronized Initiation of Two Cylindrical Rotating Detonation Engines |
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言語 |
en |
| 著者 |
Sakata, Rinpei
Inada, Masahiro
Itouyama, Noboru
Matsuoka, Ken
Kasahara, Jiro
Kawasaki, Akira
Matsuo, Akiko
Funaki, Ikkoh
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| アクセス権 |
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アクセス権 |
open access |
|
アクセス権URI |
http://purl.org/coar/access_right/c_abf2 |
| 内容記述 |
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|
内容記述タイプ |
Abstract |
|
内容記述 |
A coupled cylindrical rotating detonation engine (RDE) with two cylindrical RDEs (both combustors had a combustor inner diameter of 23 mm and an axial length of 30 mm) placed next to each other was tested for rocket clustering application. The objective of the experiment was to achieve two-engine synchronized initiation with a single igniter. Experiments were conducted on the inner wall of the combustors with different connecting-hole diameters and wall heights to evaluate the ignition delay time, combustion mode, and propulsion performance. The propellants were gaseous ethylene and oxygen, and experiments were conducted under constant conditions of mass flow rate (40±2 g/s), equivalence ratio (1.0±0.1), and backpressure (approximately 10 kPa). When the two combustion chambers were completely separated by a wall, ignition occurred with a time delay of 260 ms in the chamber without an igniter. However, when a large hole (10-mm diameter) was placed in the wall separating the two combustion chambers, synchronous initiation was successful. Synchronous initiation was also successful when the wall height was lowered (7-mm height). Under both conditions, the same level of specific impulse was achieved as for RDEs operating at the same mass flux. |
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言語 |
en |
| 内容記述 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
Published Online:20 Jun 2024 |
|
言語 |
en |
| 出版者 |
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出版者 |
American Institute of Aeronautics and Astronautics |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| 資源タイプ |
|
|
資源タイプresource |
http://purl.org/coar/resource_type/c_6501 |
|
タイプ |
journal article |
| 出版タイプ |
|
|
出版タイプ |
AM |
|
出版タイプResource |
http://purl.org/coar/version/c_ab4af688f83e57aa |
| 関連情報 |
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|
関連タイプ |
isVersionOf |
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|
識別子タイプ |
DOI |
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|
関連識別子 |
https://doi.org/10.2514/1.B39459 |
| 収録物識別子 |
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|
収録物識別子タイプ |
PISSN |
|
収録物識別子 |
0748-4658 |
| 書誌情報 |
en : Journal of Propulsion and Power
巻 40,
号 6,
p. 849-858,
発行日 2024-11
|
Papers for JPP_sakata_r4_forRepository.pdf (1.6 MB)
