Effect of hole shape on the heat transfer in a rectangular duct with perforated blockage walls

Journal of Mechanical Science and Technology

Volumn 22, Issue 10, 2008, Pages 1945-1951

  Shin, Somin ^a   Kwak, Jae Su ^a  

^a Hankuk Aviation University   (South Korea)

Author keywords

Impingement cooling; Staggered jets; Thermal performance factor; Turbine blade cooling

Indexed keywords

COOLING; ENGINES; GAS TURBINES; HEAT TRANSFER COEFFICIENTS; JETS; LIGHT SOURCES; LIQUID CRYSTALS; MIXED CONVECTION; REYNOLDS NUMBER; TURBINES; TURBOMACHINE BLADES;

CIRCULAR SHAPES; IMPINGEMENT COOLING; IMPINGEMENT JETS; INTERNAL COOLING PASSAGES; LIQUID-CRYSTAL TECHNIQUES; NUSSELT NUMBER RATIOS; RECTANGULAR DUCTS; STAGGERED JETS; THERMAL PERFORMANCE FACTOR; TURBINE BLADE COOLING; TURBINE BLADES;

HEAT EXCHANGERS;

EID: 62349094054     PISSN: 1738494X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s12206-008-0736-7     Document Type: Article

References (9)

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