Share

VISCOUS FLOW EFFECTS IN AXIAL COMPRESSORS AND TURBINES.

Author(s) : GREGORY-SMITH D. G.

Type of article: Article

Summary

PAPERS PRESENTED AT A CONFERENCE CONCENTRATED ON BOUNDARY LAYERS AS THEY AFFECT BLADE WAKES AND COMPRESSOR END WALL FLOWS. IN THE LATTER ARE INCLUDED SECONDARY FLOWS GENERATED BY TURNING THE UPSTREAM WALL BOUNDARY LAYER, THE TIP CLEARANCE LEAKAGE AND SKEW EFFECTS DUE TO THE RELATIVE MOTION OF BLADE AND END WALL. ADVANCES HAVE BEEN MADE IN THE METHODS OF CALCULATION FOR THREE-DIMENSIONAL FLOWS AND PAPERS GAVE EXAMPLES OF THIS. D.W.H.

Details

  • Original title: VISCOUS FLOW EFFECTS IN AXIAL COMPRESSORS AND TURBINES.
  • Record ID : 1983-1734
  • Languages: English
  • Source: Int. J. Heat Fluid Flow - vol. 3 - n. 3
  • Publication date: 1982
  • Document available for consultation in the library of the IIR headquarters only.

Links


See other articles in this issue (3)
See the source

Indexing