Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor

Journal of Turbomachinery

Volumn 123, Issue 1, 2001, Pages 140-146

  Van Fossen, G J ^a   Bunker, R S ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTORS; ELECTRIC HEATING; REYNOLDS NUMBER; TURBINES; TURBULENCE; VORTEX FLOW;

HOT-WIRE MEASUREMENTS;

HEAT TRANSFER;

ENGINE; HEAT TRANSFER; MEASUREMENT METHOD; TURBINE; TURBULENCE;

EID: 0034864306     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1330270     Document Type: Article

References (16)

1. Effect of turbulence level of incident air stream on local heat transfer from cylinders
2. Effects of turbulence on laminar skin friction and heat transfer
3. Effect of turbulence on heat transfer from heated cylinders
4. Experimental study of vane heat transfer and aerodynamics at elevated levels of turbulence
5. Influence of turbulence parameters, reynolds number, and body shape on stagnation region heat transfer
6. Free-stream turbulence near plane boundaries
7. Laser anemometer measurements at the exit of a T63-C20 combustor
8. Measurements of combustor velocity and turbulence profiles
9. Heat transfer distribution around nominal ice accretion shapes formed on a cylinder in the NASA lewis icing research tunnel
10. Three-dimensional flow field measurements in a transonic turbine cascade
11. Increased heat transfer to elliptical leading edges due to spanwise variations in the freestream momentum: Numerical and experimental results
12. Tables of thermal properties of gases
13. Describing uncertainties in single-sample experiments
14. A guide to uncertainty analysis of hot-wire data
15. Influence of turbulence arameters, reynolds number, and body shape on stagnation-region heat transfer