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吸込み式超音速風洞におけるスターティングロードの計測と供試体の挙動
http://hdl.handle.net/10258/00010354
http://hdl.handle.net/10258/0001035485eb37ed-bc6e-4680-a5d9-38c634a71d34
名前 / ファイル | ライセンス | アクション |
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JJSASS_56_659_580_589 (1.1 MB)
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Item type | 学術雑誌論文 / Journal Article.(1) | |||||||||||||||||
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公開日 | 2021-03-03 | |||||||||||||||||
タイトル | ||||||||||||||||||
言語 | ja | |||||||||||||||||
タイトル | 吸込み式超音速風洞におけるスターティングロードの計測と供試体の挙動 | |||||||||||||||||
言語 | ||||||||||||||||||
言語 | jpn | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | Starting Loads | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | Supersonic Wind Tunnel | |||||||||||||||||
キーワード | ||||||||||||||||||
言語 | en | |||||||||||||||||
主題Scheme | Other | |||||||||||||||||
主題 | Aerodynamic Force Measurements | |||||||||||||||||
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 | |||||||||||||||||
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 | |||||||||||||||||
著者 |
湊, 亮二郎
× 湊, 亮二郎
WEKO
752
× 溝端, 一秀
WEKO
801
× 桑田, 耕明 |
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室蘭工業大学研究者データベースへのリンク | ||||||||||||||||||
湊 亮二郎(MINATO Ryojiro) | ||||||||||||||||||
http://rdsoran.muroran-it.ac.jp/html/100000234_ja.html | ||||||||||||||||||
室蘭工業大学研究者データベースへのリンク | ||||||||||||||||||
溝端 一秀(MIZOBATA Kazuhide) | ||||||||||||||||||
http://rdsoran.muroran-it.ac.jp/html/100000207_ja.html | ||||||||||||||||||
抄録 | ||||||||||||||||||
内容記述タイプ | Abstract | |||||||||||||||||
内容記述 | Measurements of starting load in the indraft supersonic wind tunnel of Muroran Institute of Technology were conducted for Mach 2, 3 and 4 conditions with AGARD-B model. The high speed photographs were taken for the behaviors of the wind tunnel model. Those photographs make clear that the oscillations of the model coincide with the measured starting load oscillation and starting loads were caused by two shock waves. The first shock wave is the reflection shock, which is generated at the nozzle throat by expansion wave reflection. The second one is asymmetric oblique shock waves (AOS) coming from the upstream. AOS can generate the asymmetric conical shock (ACS) around the nose cone of the model, which would have directly caused the starting loads on the wind tunnel model. Based on those observations, the authors presented the conical shock theory, which is the alternative starting load prediction theory to the normal shock theory. | |||||||||||||||||
言語 | en | |||||||||||||||||
書誌情報 |
ja : 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences 巻 56, 号 659, p. 580-589, 発行日 2008-12-05 |
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出版者 | ||||||||||||||||||
言語 | ja | |||||||||||||||||
出版者 | 日本航空宇宙学会 | |||||||||||||||||
出版者版へのリンク | ||||||||||||||||||
10.2322/jjsass.56.580 | ||||||||||||||||||
https://doi.org/10.2322/jjsass.56.580 | ||||||||||||||||||
DOI | ||||||||||||||||||
関連タイプ | isIdenticalTo | |||||||||||||||||
識別子タイプ | DOI | |||||||||||||||||
関連識別子 | 10.2322/jjsass.56.580 | |||||||||||||||||
日本十進分類法 | ||||||||||||||||||
主題Scheme | NDC | |||||||||||||||||
主題 | 538 | |||||||||||||||||
ISSN | ||||||||||||||||||
収録物識別子タイプ | PISSN | |||||||||||||||||
収録物識別子 | 13446460 | |||||||||||||||||
権利 | ||||||||||||||||||
言語 | ja | |||||||||||||||||
権利情報 | © 2008 日本航空宇宙学会 | |||||||||||||||||
著者版フラグ | ||||||||||||||||||
出版タイプ | VoR | |||||||||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||||||||
フォーマット | ||||||||||||||||||
内容記述タイプ | Other | |||||||||||||||||
内容記述 | application/pdf |