Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn / David L. Rigby.
- Physical Description: 1 online resource (12 pages) : illustrations.
- Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1999.
"Prepared for the 43rd Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Stockholm, Sweden, June 2-5, 1998."
"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
|Bibliography, etc. Note:||
Includes bibliographical references (pages 11-12).
|Type of Report and Period Covered Note:||
|Funding Information Note:||
Sponsored by the National Aeronautics and Space Administration WU-523-26-13-00 E-11300
|Source of Description Note:||
Description based on online resource; title from PDF title page (NASA, viewed Aug. 21, 2017).
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