Film cooling effectiveness from trenched shaped and compound holes
Author:
Publisher
Springer Science and Business Media LLC
Subject
Fluid Flow and Transfer Processes,Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s00231-007-0341-9.pdf
Reference34 articles.
1. Garg VK (1999) Heat transfer on a film-cooled rotating blade. NASA/CR-1999-209301 report
2. Bunker RS (2005) A review of shaped hole turbine film-cooling technology. J Heat Transf 127:441–453
3. Bogard DG, Thole KA (2006) Gas turbine cooling. J Propulsion Power 22(2)
4. Han JC, Teng S (2000) Effect of film-hole shape on turbine blade film cooling performance. NASA/CR–2000-209932
5. Schmidt DL, Sen B, Bogard DG (1996) Film cooling with compound angle holes: adiabatic effectiveness. J Turbomach 118:807–813
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