低レイノルズ数におけるNACA0012翼の伴流特性 : 迎角の急変化に対する伴流の過渡現象(G05-6 内部流れ・境界層(2),G05 流体工学部門一般講演)
スポンサーリンク
概要
- 論文の詳細を見る
Many researchers have attracted attention in the study of fluid mechanics at low Reynolds numbers (10^2<Re<10^4). We also interested in wake-flow characteristics of this region behind a wing, which can be altered from a streamlined-to a bluff-body by changing its angle of attack. Measurements were made of mean velocity profiles using hot-wire technique in the transitional wake-flow field produced by an aerofoil of NACA0012 when its angle of attack changed impulsively from zero to arbitrary angle at chord-Reynolds numbers from 700 to 1700. As a result, it was found that the wake-flow behavior in the transitional term was different in every Reynolds number and angle of attack.
- 2004-09-04
論文 | ランダム
- 中国の大学教育改革と学生の教育経験の変化 : 北京大学,清華大学,復旦大学を事例分析として
- 畜舎排水の現状と対策
- 規格試験方法とその意義(ATF)
- Forssman glycosphingolipid as an immunohistochemical marker for mouse stromal macrophages in hemopoietic foci
- Bone metabolism after cessation of long-term hormone replacement therapy for postmenopausal osteoporosis (第20回婦人科骨粗鬆症研究会) -- (治療)