The variation of heat transfer coefficient, adiabatic effectiveness and aerodynamic loss with film cooling hole shape

Annals of the New York Academy of Sciences

Volumn 934, Issue , 2001, Pages 361-368

  Sargison, J E ^a   Guo, S M ^a   Oldfield, M L G ^a   Rawlinson, A J ^b  

^a UNIVERSITY OF OXFORD   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFLOW; CONFERENCE PAPER; COOLING; DYNAMICS; FILM; FLOW RATE; GEOMETRY; HEAT TRANSFER; STEADY STATE;

EID: 0034952040     PISSN: 00778923     EISSN: None     Source Type: Book Series    
DOI: 10.1111/j.1749-6632.2001.tb05871.x     Document Type: Conference Paper

References (6)

1. Film cooling
2. The influence of film cooling on the efficiency of an annular nozzle guide vane cascade
3. Definition of heat transfer coefficient in the turbine situation
4. Aerodynamic performance of an annular cascade of film cooled nozzle guide vanes under engine representative conditions