抄録
A detailed experimental investigation was carried out to examine the three-dimensional boundary layer characteristics in a radial inflow turbine scroll. Some basic flow phenomena and growth of secondary flow were also investigated. In the inlet region of the scroll, the incoming boundary layer begins to have the skewed nature, namely the radially inward secondary flow caused by the radial pressure gradient. From the inlet region to the one third of the scroll circumference, the secondary flow grows so strongly that the most of the low momentum fluid in the incoming boundary layer are transported to the nozzle region.
| 元の言語 | 英語 |
|---|---|
| ジャーナル | American Society of Mechanical Engineers (Paper) |
| 出版物ステータス | 出版済み - 1 1 1993 |
| イベント | International Gas Turbine and Aeroengine Congress and Exposition - Cincinnati, OH, USA 継続期間: 5 24 1993 → 5 27 1993 |
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All Science Journal Classification (ASJC) codes
- Mechanical Engineering
これを引用
Behavior of three-dimensional boundary layers in a radial inflow turbine scroll. / Hara, Kazuo; Furukawa, Masato; Inoue, Masahiro.
：: American Society of Mechanical Engineers (Paper), 01.01.1993.研究成果: ジャーナルへの寄稿 › Conference article
}
TY - JOUR
T1 - Behavior of three-dimensional boundary layers in a radial inflow turbine scroll
AU - Hara, Kazuo
AU - Furukawa, Masato
AU - Inoue, Masahiro
PY - 1993/1/1
Y1 - 1993/1/1
N2 - A detailed experimental investigation was carried out to examine the three-dimensional boundary layer characteristics in a radial inflow turbine scroll. Some basic flow phenomena and growth of secondary flow were also investigated. In the inlet region of the scroll, the incoming boundary layer begins to have the skewed nature, namely the radially inward secondary flow caused by the radial pressure gradient. From the inlet region to the one third of the scroll circumference, the secondary flow grows so strongly that the most of the low momentum fluid in the incoming boundary layer are transported to the nozzle region.
AB - A detailed experimental investigation was carried out to examine the three-dimensional boundary layer characteristics in a radial inflow turbine scroll. Some basic flow phenomena and growth of secondary flow were also investigated. In the inlet region of the scroll, the incoming boundary layer begins to have the skewed nature, namely the radially inward secondary flow caused by the radial pressure gradient. From the inlet region to the one third of the scroll circumference, the secondary flow grows so strongly that the most of the low momentum fluid in the incoming boundary layer are transported to the nozzle region.
UR - http://www.scopus.com/inward/record.url?scp=0027262877&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0027262877&partnerID=8YFLogxK
M3 - Conference article
AN - SCOPUS:0027262877
JO - American Society of Mechanical Engineers (Paper)
JF - American Society of Mechanical Engineers (Paper)
SN - 0402-1215
ER -