Blade heat transfer measurements and predictions in a transonic turbine cascade /

Bibliographic Details
Main Author:	Giel, P. W. (Paul W.) (Author)
Corporate Author:	U.S. Army Research Laboratory
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center : U.S. Army Research Laboratory, August 1999.
Series:	NASA technical memorandum ; 1999-209296. ARL-TR (Aberdeen Proving Ground, Md.) ; 2029.
Subjects:	Heat transfer. Heat measurement. Supersonic turbines. Rotor stator interactions. Rotor blades (turbomachinery)
Online Access:	https://purl.fdlp.gov/GPO/gpo86573

Description
Item Description:	"August 1999." "Prepared for the 1999 International Gas Turbine and Aeroengine Congress cosponsored by the American Society of Mechanical Engineers and the International Gas Turbine Institute, Indianapolis, Indiana, June 7-10, 1999." "Performing organization: NASA Glenn Research Center and U.S. Army Research Laboratory"--Report documentation page. Description based on online resource; title from PDF title page (NASA, viewed Nov. 20, 2017).
Physical Description:	1 online resource (15 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 14-15).