Endwall heat transfer measurements in an annular cascade of nozzle guide vanes at engine representative Reynolds and Mach numbers-Reference-Cited by-同舟云学术

Endwall heat transfer measurements in an annular cascade of nozzle guide vanes at engine representative Reynolds and Mach numbers

Published:1996-04 Issue:2 Volume:17 Page:139-147
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:

Spencer M.C.,Jones T.V.,Lock G.D.

Publisher

Elsevier BV

Subject

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

Reference20 articles.

1. Effects of simulated combustor turbulence on boundary layer heat transfer;Ames;ASME HTD,1990

2. Heat transfer and aerodynamics of high rim speed turbine nozzle guide vane with profiled end-walls;Chana;ASME Paper 92-GT-243,1992

3. Temperature ratio effects in compressible turbulent boundary layers;Fitt;Int. J. Heat Mass Transfer,1986

4. The application of thin film gauges on flexible plastic substrates to the gas turbine situation;Guo;ASME Paper 95-GT-357,1995

5. Heat transfer and aerodynamics of a high rim speed turbine nozzle guide vane tested in the RAE isentropic light piston cascade (ILPC);Harasgama;ASME Paper 90-GT-41,1990

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