Full-coverage film cooling with short normal injection holes

Journal of Turbomachinery

Volumn 123, Issue 4, 2001, Pages 798-805

  Harrington, M K ^a   McWaters, M A ^a   Bogard, D G ^a   Lemmon, C A ^a   Thole, K A ^a  

^a The University of Texas at Austin   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLOW MOLDING; COOLANTS; TURBULENCE;

INJECTION HOLES;

COOLING;

AEROSPACE; COOLING; ENGINE; PERFORMANCE ASSESSMENT; TURBINE;

EID: 0035484059     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1400111     Document Type: Article

References (12)

1. Heat (Mass) transfer and film cooling effectiveness with injection through discrete holes: Part II - On the exposed surface
2. Effectiveness and heat transfer with full-coverage film cooling
3. Multihole cooling film effectiveness and heat transfer
4. Heat transfer with film cooling within and downstream of one to four rows of normal injection holes
5. Film cooling effectiveness for injection from multirow holes
6. Gaseous film cooling with multiple injection stations
7. Film cooling for short film cooling holes fed by a narrow plenum
8. Generating high freestream turbulence levels
9. Highly turbulent mainstream effects on film cooling of a simulated airfoil leading edge
10. Describing the uncertainties in experimental results