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

Bibliographic Details

Main Authors:	VanFossen, G. James (Author), Bunker, Ronald S. (Author)
Format:	Government Document 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:	https://purl.fdlp.gov/GPO/LPS30203