Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor
By: G. James Van Fossen, Ronald S. Bunker.
Contributors: Bunker, Ronald S.; NASA Glenn Research Center.
Series: NASA/TM -- 2000-210241.; NASA technical memorandum -- 210241.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information
Published: 2000
Place of publication: Cleveland, Ohio; Hanover, MD
Language: eng
Format: Microform
Subjects: Augmentation.; Stagnation point.; Flow distribution.; Heat transfer.; Gas turbines.; Turbulent flow.; Isotropic turbulence.
Notes: Shipping list no.: 2002-0367-M.

"July 2000."

Also available via Internet from the NASA web site. Address as of 4/28/03: http://gltrs.grc.nasa.gov/reports/2000/TM-2000-210241.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.