Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor /

Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor /

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Bibliographic Details
Main Authors: VanFossen, G. James (Author), Bunker, Ronald S. (Author)
Format: Government Document Electronic eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2000.
Series:NASA technical memorandum ; 2000-210241.
Subjects:
Augmentation.
Stagnation point.
Flow distribution.
Heat transfer.
Gas turbines.
Turbulent flow.
Isotropic turbulence.
Online Access:CONNECT
Description
Item Description:"July 2000."
"Prepared for the 45th International Gas Turbine and Aeroengine Technical Congress sponsored by the American Society of Mechanical Engineers, Munich, Germany, May 8-11, 2000."
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
"ASME 2000-GT-0215."
Physical Description:1 online resource (9 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 8-9).

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