A converging slot-hole film-cooling geometry Part 2: Transonic nozzle guide vane heat transfer and loss

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2001, Pages

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

^a UNIVERSITY OF OXFORD   (United Kingdom)

^b University of Bath   (United Kingdom)

^c ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COOLANTS; COOLING; ENGINES; HEAT FLUX; LIQUID CRYSTALS; NOZZLES; REYNOLDS NUMBER; STEREOLITHOGRAPHY; TRANSONIC AERODYNAMICS;

AERO-DYNAMIC PERFORMANCE; AERODYNAMIC EFFICIENCY; ANALYSIS TECHNIQUES; EFFICIENCY MEASUREMENT; ENGINE TEMPERATURES; MOMENTUM FLUX RATIOS; SURFACE HEAT TRANSFER COEFFICIENT; THERMOCHROMIC LIQUID CRYSTALS;

GEOMETRY;

EID: 84905728362     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2001-GT-0127     Document Type: Conference Paper

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