並列タイトル等Three-Dimensional Boundary-Layer Transition on a Swept Cylinder
タイトル(掲載誌)航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-15
一般注記An experiment has been carried out on three-dimensional boundary-layer transition along a swept cylinder with a diameter of 500 mm. The surface-oil-flow technique has been used to study the development of stationary vortices, which are characteristic of cross-flow instability. Hot-wire anemometer surveys show that two kinds of time-dependent disturbances grow prior to turbulent state. The first disturbance may be ascribed to T-S wave-type instability. The following second with one order higher frequency than that of the first is caused by inflectional instability. There is no incongruity between experimental and current theoretical results.
資料番号: NALSP0015008
レポート番号: NAL SP-15
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43482&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース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