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ムービングベルト式地面効果試験装置
https://jaxa.repo.nii.ac.jp/records/40182
https://jaxa.repo.nii.ac.jp/records/40182029660fa-0e43-41c4-9758-b5bf8aab07b5
名前 / ファイル | ライセンス | アクション |
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naltm0000724.pdf (757.4 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ムービングベルト式地面効果試験装置 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地面効果試験装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ムービングベルト装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ベルト走行特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 気流特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層吸込 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 静圧分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱れ分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地面板 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ground effect testing system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low speed wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | moving belt system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | belt running characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer suction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | static pressure distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulent distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ground plane | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Moving belt ground effect testing system of NAL 6.5 x 5.5 m low speed wind tunnel | |||||
著者 |
野中, 修
× 野中, 修× 萱場, 重男× 林, 良生× Nonaka, Osamu× Kayaba, Shigeo× Hayashi, Yoshio |
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著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所資料 en : Technical Memorandum of National Aerospace Laboratory 巻 724, p. 1-30, 発行日 1998-02 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 航空機模型の離着陸時の地面効果を評価するために、ムービングベルト式の地面効果試験装置が1995年3月に大型低速風洞に完成した。ここでは、本装置の構成と特性について述べる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A moving belt type ground effect measurement system was constructed to evaluate ground effect characteristics of aircraft models at the NAL low speed wind tunnel facility in March 1995. This paper summarizes the hardware and function of this equipment. Some function tests and flow characteristic tests were carried out, with this equipment installed in the test section. Some effects of the following parameters to drive this system on the flow above the belt plane are indicated: (1) belt running speed; (2) boundary layer suction; and (3) rear flap of ground plane. These parameters were adjusted to the optimum values experimentally. Some experimental results on the following items are indicated: (1) static pressure distribution along the wind tunnel axis on the moving plane; (2) turbulent distribution on the moving plane; and (3) boundary layer velocity profile on the moving plane. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001439000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TM-724 |