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Effects of simulated combustor turbulence on boundary layer heat transferA simulated combustor flow field has been generated in order to study the effects of high intensity large scale turbulence on boundary layer heat transfer. Turbulence intensities of up to 19 percent and integral lengths scales of 4 to 6 centimeters have been generated. Heat transfer has been augmented by up to 28 percent for the flat plate constant velocity turbulent boundary layer.
Document ID
19930070625
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Ames, F. E.
(NASA Headquarters Washington, DC United States)
Moffat, R. J.
(Stanford Univ. CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1990
Publication Information
Publication: In: Heat transfer in turbulent flow (A93-54620 24-34)
Publisher: American Society of Mechanical Engineers
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
93A54622
Distribution Limits
Public
Copyright
Other

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