Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating /

Bibliographic Details
Main Author:	Shyam, Vikram
Corporate Authors:	ASME Turbo Expo, NASA Glenn Research Center
Other Authors:	Ameri, Ali
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA technical memorandum ; 2012-217607.
Subjects:	Computational fluid dynamics. Supersonic turbines. Blade tips. Supersonic flow. Rotor aerodynamics. Axial flow turbines. Supersonic heat transfer. Contours.
Online Access:	https://purl.fdlp.gov/GPO/gpo31866

Description
Item Description:	Title from title screen (viewed on Dec. 3, 2012). "July 2012." "Prepared for the TURBO EXPO 2011 sponsored by the American Society of Mechanical Engineers (ASME) Vancouver, British Columbia, June 6-10, 2011." "GT2011-46390." Electronic resource.
Physical Description:	1 online resource (8 pages) : illustrations (some color).
Bibliography:	Includes bibliographical references (page 8).