Research on Diagonal-Inflow Turbine with High Specific Speed (1st Report, Aerodynamic Performance of Airfoil Impeller)

Masahiro Inoue, Masato Furukawa, Kazuo Hara, Shikho Kiyota

研究成果: ジャーナルへの寄稿記事

抄録

In order to develop a diagonal inflow gas turbine with a three-dimensional airfoil impeller, an experimental investigation was carried out. For that purpose, an airfoil impeller was made on the basis of a quasi-three-dimensional design, and the internal flow field was measured in detail. It was found that the diagonal inflow turbine with a three-dimensional airfoil impeller can be operated efficiently at high specific speed, and that the velocity coefficient of the impeller is as high as that for an axial flow turbine. But the turbine performance is strongly affected by the secondary flow in the impeller, which is so strong that the low energy fluid is accumulated near the tip of impeller. It is necessary to study on determination of the optimum incidence angle by considering this secondary flow.

元の言語英語
ページ(範囲)2843-2847
ページ数5
ジャーナルTransactions of the Japan Society of Mechanical Engineers Series B
50
発行部数459
DOI
出版物ステータス出版済み - 1 1 1984
外部発表Yes

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airfoils
turbines
Airfoils
aerodynamics
Aerodynamics
secondary flow
Turbines
Secondary flow
axial flow turbines
internal flow
Axial flow
gas turbines
Gas turbines
Flow fields
flow distribution
incidence
Fluids
fluids
coefficients
energy

All Science Journal Classification (ASJC) codes

  • Condensed Matter Physics
  • Mechanical Engineering

これを引用

Research on Diagonal-Inflow Turbine with High Specific Speed (1st Report, Aerodynamic Performance of Airfoil Impeller). / Inoue, Masahiro; Furukawa, Masato; Hara, Kazuo; Kiyota, Shikho.

:: Transactions of the Japan Society of Mechanical Engineers Series B, 巻 50, 番号 459, 01.01.1984, p. 2843-2847.

研究成果: ジャーナルへの寄稿記事

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