Investigation of the Purge Process on the Multi-Cycle Operations of a Pulse Detonation Engine
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- SAKURAI Takashi
- Graduate School of Science and Engineering, Saitama University
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- OOKO Akinori
- Graduate School of Science and Engineering, Saitama University
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- YOSHIHASHI Teruo
- Department of Mechanical Engineering, Saitama University
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- OBARA Tetsuro
- Department of Mechanical Engineering, Saitama University
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- OHYAGI Shigeharu
- Department of Mechanical Engineering, Saitama University
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抄録
The pulse detonation engine (PDE) is a propulsion system that generates thrust by repetitive detonation. Performance of the PDE, such as specific impulse, has gained much attention. However, the details of operational conditions related to performance have not been clarified. In this study, to investigate these issues, a hydrogen-air PDE was constructed and the effect of the purge process on multi-cycle operations was studied. The exhaust of the burned gas from the PDE was made by rarefaction waves so that it is expected not to create internal disturbance, such as spiral, in the tube so that the burned gas can be exhausted smoothly. A purge process using air was applied to assist the exhaust process in order to prevent failures in multi-cycle operations. The effects of the purge-volume fraction were investigated. As a result, when a purge-air gas filled the region including the spark plug, detonations occurred in a stable manner. Using these conditions, multi-cycle experiments ranging from 10 to 50 Hz were conducted and profiles of the thrust-wall pressure are discussed in detail.
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 48 (160), 78-85, 2005
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001204079953152
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- NII論文ID
- 10016766214
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- NII書誌ID
- AA0086707X
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- ISSN
- 21894205
- 05493811
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- NDL書誌ID
- 7388628
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可