Turbulent heat transfer and friction in a segmental channel that simulates leading-edge cooling channels of modern turbine blades /

2.0, 4.0, 6.0, and infinity, and mass flow rates

Bibliographic Details

Main Author:	Spence, Rodney Brian
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 1995.
Subjects:	Major mechanical engineering.
Online Access:	Link to OAKTrust copy