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Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn Preview this item
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Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn

Author: D L Rigby; Lewis Research Center,
Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1999.
Series: NASA technical memorandum, 1999-208501.
Edition/Format:   eBook : Document : National government publication : EnglishView all editions and formats
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Genre/Form: Online resources
Additional Physical Format: Print version:
Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn
(OCoLC)213890627
Microfiche version:
Rigby, D.L. (David Lester), 1963-
Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn
(OCoLC)42042478
Material Type: Document, Government publication, National government publication, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: D L Rigby; Lewis Research Center,
OCLC Number: 1001438248
Notes: "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.
Description: 1 online resource (12 pages) : illustrations.
Series Title: NASA technical memorandum, 1999-208501.
Responsibility: David L. Rigby.

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