Effects of Mach number and Reynolds number on jet array impingement heat transfer

International Journal of Heat and Mass Transfer

Volumn 50, Issue 1-2, 2007, Pages 367-380

  Goodro, Matt ^a,b   Park, Jongmyung ^a,b   Ligrani, Phil ^a,b,d   Fox, Mike ^c   Moon, Hee Koo ^c  

^a University of Utah   (United States)

^b UNIVERSITY OF UTAH   (United States)

^c SOLAR TURBINES INCORPORATED   (United States)

^d UNIVERSITY OF OXFORD   (United Kingdom)

Author keywords

Gas turbines; Heat transfer augmentation; Impingement cooling; Internal cooling

Indexed keywords

COOLING; DISCHARGE (FLUID MECHANICS); GAS TURBINES; HEAT TRANSFER; NUSSELT NUMBER; REYNOLDS NUMBER;

HEAT TRANSFER AUGMENTATION; IMPINGEMENT COOLING; INTERNAL COOLING;

JETS;

COOLING; DISCHARGE (FLUID MECHANICS); GAS TURBINES; HEAT TRANSFER; JETS; NUSSELT NUMBER; REYNOLDS NUMBER;

EID: 33751213602     PISSN: 00179310     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijheatmasstransfer.2006.06.007     Document Type: Article

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