Film cooling from a row of holes supplemented with antivortex holes

Journal of Turbomachinery

Volumn 131, Issue 2, 2009, Pages

  Dhungel, Alok ^a   Lu, Yiping ^a   Phillips, Wynn ^a   Ekkad, Srinath V ^b   Heidmann, James ^c  

^a Louisiana State University   (United States)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANTIVORTEX; BLOWING RATIO; CIRCULAR CROSS-SECTIONS; COOLING PERFORMANCE; CYLINDRICAL HOLES; FILM COOLING; FILM COOLING EFFECTIVENESS; FILM COOLING HOLE; FILM COOLING PERFORMANCE; FILM HOLES; FREE-STREAM VELOCITY; GLENN RESEARCH CENTER; IR THERMOGRAPHY; UPSTREAM REGION;

DESIGN; HEAT EXCHANGERS; HEAT TRANSFER COEFFICIENTS; NASA; REYNOLDS NUMBER;

COOLING;

EID: 77955165729     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2950059     Document Type: Article

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