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Bibliographic Record
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- Material Type
- 規格・テクニカルリポート類
- Author/Editor
- 杉浦, 裕樹吉田, 憲司徳川, 直子高木, 正平西沢, 啓Sugiura, HirokiYoshida, KenjiTokugawa, NaokoTakagi, ShoheiNishizawa, Akira
- Author Heading
- Publication, Distribution, etc.
- Publication Date
- 2000-12
- Publication Date (W3CDTF)
- 2000-12
- Alternative Title
- 超音速輸送機向け無推力実験機の自然層流翼上の遷移測定
- Periodical title
- 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory
- No. or year of volume/issue
- 48T
- Volume
- 48T
- Pages
- 51-54
- ISSN (Periodical Title)
- ISSN : 0289-260X
- Text Language Code
- eng
- Subject Heading
- Target Audience
- 一般
- Note (General)
- 出版タイプ： NA航空宇宙技術研究所 27-29 Sept.2000 東京 日本National Aerospace Laboratory 27-29 Sept.2000 Tokyo Japan超音速輸送機を目的とした無推力実験機の自然層流翼上の遷移測定をマッハ数2.0と1.2で行った。翼弦沿いに設置した熱フィルム流速計に対する出力信号の振幅中の摂動増加が層流から乱流境界層への遷移を示す。熱フィルム流速計およびPreston管による測定結果は遷移点が翼の半弦の下流に位置していることを明らかにした。Transition measurement on the natural laminar flow wing of non-powered experimental airplane for supersonic transport was conducted at Mach 2.0 and 1.2. Increase of perturbation in amplitude of output signals for hot-films placed along the wing chord indicates transition from laminar to turbulent boundary layer. Results by hot-film and Preston tubes proved that transition point is located downstream of the half chord of the wing.資料番号: AA0028637019レポート番号: NAL SP-48T
- Periodical Title (NCID)
- AN10097345
- Data Provider (Database)
- 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
- Original Data Provider (Database)
- 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ