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.
|General Note:|| "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:|| Technical memorandum.
|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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