Film cooling from rows of holes - Effect of cooling hole shape and row arrangement on adiabatic effectiveness

Annals of the New York Academy of Sciences

Volumn 934, Issue , 2001, Pages 321-328

  Dittmar, J ^a   Jung, I S ^b   Schulz, A ^a   Wittig, S ^a   Lee, J S ^a  

^a UNIVERSITY OF KARLSRUHE   (Germany)

^b Seoul National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

CONFERENCE PAPER; COOLING; FILM; MATHEMATICAL MODEL; THERMOGRAPHY; TURBULENT FLOW; VELOCITY;

EID: 0034956064     PISSN: 00778923     EISSN: None     Source Type: Book Series    
DOI: 10.1111/j.1749-6632.2001.tb05866.x     Document Type: Conference Paper

References (12)

1. Adiabatic wall temperature and heat transfer downstream of injection through two rows of holes
2. Film cooling from two rows of holes inclined in the streamwise and spanwise directions
3. Film cooling and heat transfer from a combination of two rows of simple and / or compound angle holes in inline and / or staggered configurations
4. Film-cooling from holes with compound angle orientations: Part 1 - Results downstream of two staggered rows of holes with 3d spanwise spacing
5. Effects of hole geometry and density on three-dimensional film cooling