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Effect of free-stream turbulence on film coolingFilm-cooling experiments were conducted at four levels of free-stream turbulence to test the hypothesis that the film-cooling effectiveness is inversely related to the free-stream turbulence level. The hot-gas operating conditions were held constant at a temperature of 590 K, a pressure of 1 atmosphere, and a velocity of 62 m/sec. The film-cooling air was at ambient inlet temperature, and the film-cooling flow rates were 2.5, 5.0, 7.5, and 10.0 percent of the total airflow. Blockage plates with blockage areas of 0, 52, 72, and 90 percent were placed upstream of the film-cooling slot and produced axial turbulence intensities of 7, 14, 23, and 35 percent, respectively. The film-cooling effectiveness decreased as much as 50 percent as the freestream turbulence intensity was increased from 7 to 35 percent. The value of the turbulent mixing coefficient used in previous work was compared with the axial turbulence intensity. The turbulent mixing coefficient was found to be 10 to 40 percent of the axial turbulence intensity.
Document ID
19750017021
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Marek, C. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Tacina, R. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TN-D-7958
E-8188
Report Number: NASA-TN-D-7958
Report Number: E-8188
Accession Number
75N25093
Funding Number(s)
PROJECT: RTOP 505-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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