Exit plane and suction surface flows in an annular turbine cascade with a skewed inlet boundary layer-Reference-Cited by-同舟云学术

Exit plane and suction surface flows in an annular turbine cascade with a skewed inlet boundary layer

Published:1980-06 Issue:2 Volume:2 Page:57-66
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Bindon Jeffery P.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference11 articles.

1. Skewed boundary layer flow near the endwalls of a compressor cascade;Moore;Trans. ASME,1957

2. Secondary flow and losses in turbine cascade with inlet skew;Carrick;Agardograph,1977

3. The endwall boundary layer in an annular cascade of turbine nozzle guide vanes;Sjolander,1975

4. BINDON, J. P. ‘The effect of hub inlet boundary layer skewing on the endwall shear flow in an annular turbine cascade’, A.S.M.E. paper No. 79-GT-17

5. BINDON, J. P., ABURWIN, B. A., and MACCALLUM, N.R.L. ‘Comparison of transverse injection effects in straight and in annular cascades’, A.S.M.E., paper No. 79-GT-13

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