Computational study of turbine blade cooling by slot-injection of a gas-Reference-Cited by-同舟云学术

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Computational study of turbine blade cooling by slot-injection of a gas

Published:1997-12 Issue:12 Volume:17 Page:1141-1149
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Kadja Mahfoud,Bergeles George

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference15 articles.

1. The aerodynamic penalties associated with blade cooling;Barry,1976

2. Film cooling;Goldstein;Adv. Heat Trans.,1971

3. Aerodynamics of slot-film cooling: theory and experiment;Fitt;J. Fluid Mech.,1985

4. Slot-film cooling—the effect of separation angle;Fitt;Acta Mechanica,1994

5. On slot injection into a supersonic laminar boundary layer;Smith,1973

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical investigation of the intercooler of a two-stage refrigerant compressor;Applied Thermal Engineering;2007-10

2. Temperature-related errors on aerofoil section of turbine blade;Journal of Materials Processing Technology;2001-09

3. Heat transfer — a review of 1997 literature;International Journal of Heat and Mass Transfer;2000-07

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