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Repetitive Energy Deposition at a Supersonic Intake in Subcritical and Buzz Modes
http://hdl.handle.net/2237/00032253
http://hdl.handle.net/2237/00032253416dea58-9a90-4bb9-8322-4dc12860acbf
名前 / ファイル | ライセンス | アクション |
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AIAAJ-J058519_FINALED_2s (2.6 MB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2020-05-26 | |||||
タイトル | ||||||
タイトル | Repetitive Energy Deposition at a Supersonic Intake in Subcritical and Buzz Modes | |||||
言語 | en | |||||
著者 |
Myokan, Manabu
× Myokan, Manabu× Kubota, Akiya× Iwakawa, Akira× Sasoh, Akihiro |
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アクセス権 | ||||||
アクセス権 | open access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||
権利 | ||||||
言語 | en | |||||
権利情報 | Copyright © 2019 by Manabu Myokan, Akiya Kubota, Akira Iwakawa, and Akihiro Sasoh. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | This study experimentally investigated the effects of repetitive laser energy deposition using a supersonic intake model with a central conical compression surface and a 19×19 mm^2 cross-sectional duct in a Mach 1.92 indraft wind tunnel: especially in the subcritical and buzz modes. A single-pulse energy deposition was observed to suppress the flow separation at the compression surface by “sweeping” a shock wave system with the thermal bubble generated by the energy deposition. The duration of the sweeping effect was approximately 160 μs in the subcritical mode and 100–420 μs in the buzz mode. Furthermore, repetitive deposition of laser pulse energies was observed to moderate instabilities in both modes, and it increased the pressure recovery by as much as 8%; also, the occurrence of buzz was delayed, thereby widening the stable, subcritical regime. In both modes, there was a threshold value for the laser pulse repetition frequency fL, thd, which corresponded to the duration of the sweeping effect (e.g., fthd=6 kHz in subcritical mode). Below this frequency, the increase in the pressure was proportional to the repetition frequency; whereas above fthd, the effect per single pulse was reduced. | |||||
言語 | en | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | Published Online:26 Oct 2019 | |||||
言語 | en | |||||
出版者 | ||||||
出版者 | American Institute of Aeronautics and Astronautics | |||||
言語 | en | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | 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 | |||||
DOI | ||||||
関連タイプ | isVersionOf | |||||
識別子タイプ | DOI | |||||
関連識別子 | https://doi.org/10.2514/1.J058519 | |||||
ISSN(print) | ||||||
収録物識別子タイプ | PISSN | |||||
収録物識別子 | 0001-1452 | |||||
書誌情報 |
en : AIAA Journal 巻 58, 号 1, p. 107-117, 発行日 2020-01 |
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著者版フラグ | ||||||
値 | author |