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

Bibliographic Details

Main Author:	VanFossen, G. James
Corporate Author:	NASA Glenn Research Center
Other Authors:	Bunker, Ronald S.
Format:	Government Document Book
Language:	English
Published:	Cleveland, Ohio : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, [2000]
Series:	NASA technical memorandum ; 210241.
Subjects:	Augmentation. Stagnation point. Flow distribution. HEAT TRANSFER. GAS TURBINES. Turbulent flow. Isotropic turbulence.
Online Access:	Adobe Acrobat Reader required