Heat transfer near turbine nozzle endwall

Annals of the New York Academy of Sciences

Volumn 934, Issue , 2001, Pages 27-36

  Chyu, M K ^a  

^a University of Pittsburgh   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANALYTIC METHOD; COMBUSTION; CONFERENCE PAPER; COOLING; FILM; FLOW RATE; HEAT TRANSFER; TURBULENT FLOW;

EID: 0034953626     PISSN: 00778923     EISSN: None     Source Type: Book Series    
DOI: 10.1111/j.1749-6632.2001.tb05840.x     Document Type: Conference Paper

References (32)

1. Crossflows in a turbine cascade passage
2. Turbulent transport on the endwall in the region between adjacent turbine blades
3. Comparison of visualized turbine endwall secondary flows and measured Heat transfer patterns
4. Influence of mach number and end wall cooling on secondary flows in a straight nozzle cascade
5. Aerodynamics of cooling jets introduced in the secondary flow of a low speed turbine cascade
6. Film cooling research on the endwall of a turbine nozzle guide vane in a short duration annular cascade part 1: Experimental technique and results
7. Distribution of film-cooling effectiveness on a turbine endwall measured using ammonia and diazo technique
8. Aerodynamic aspects of endwall film-cooling
9. An experimental study of heat transfer and film cooling on large-scale turbine endwalls
10. Experimental investigation of endwall profiling in a turbine vane cascade
11. A rare-earth phosphor laser-induced fluorescence thermal imaging system