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

この論文をさがす

著者

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 Int. J.

    JSME Int. J. 33(2), 265-271, 1990

    一般社団法人日本機械学会

被引用文献:  3件中 1-3件 を表示

各種コード

  • NII論文ID(NAID)
    110002492494
  • NII書誌ID(NCID)
    AA10680596
  • 本文言語コード
    ENG
  • 資料種別
    雑誌論文
  • ISSN
    09148817
  • データ提供元
    CJP引用  NII-ELS 
ページトップへ