Performance of the Wells Turbine with a Double Row of Guide Vanes

• GATO L. M. C.

• FALCAO A. F. de O.

抄録

The paper describes a theoretical and experimental investigation concerning the aerodynamic performance of the Wells turbine, in which a stationary blade row is added on each side of the rotor. The entire blade system is symmetrical with respect to a plane perpendicular to the turbine axis. A quasi-three-dimensional flow analysis is developed and used to design and build a turbine model. Experimental as well as theoretically predicted values are presented and indicate that the presence of stationary blades can provide a considerable increase in efficiency.

収録刊行物

• JSME international journal. Ser. 2, Fluids engineering, heat transfer, power, combustion, thermophysical properties

  JSME international journal. Ser. 2, Fluids engineering, heat transfer, power, combustion, thermophysical properties 33 (2), 265-271, 1990

  一般社団法人 日本機械学会

キーワード

• Turbomachinery
• Wells Turbine
• Wave Energy

詳細情報

• CRID: 1390282680403748480
• NII論文ID: 110002492494
• NII書誌ID: AA10680596
• DOI: 10.1299/jsmeb1988.33.2_265
• ISSN: 09148817
• Web Site: https://www.jstage.jst.go.jp/article/jsmeb1988/33/2/33_2_265/_pdf
• 本文言語コード: en
• データソース種別:
  • JaLC
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可