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