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

Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating [electronic resource] / Vikram Shyam, Ali Ameri.

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Bibliographic Details
Online Access:	Online Access Online Access
Main Author:	Shyam, Vikram
Corporate Authors:	NASA Glenn Research Center, ASME Turbo Expo
Other Authors:	Ameri, Ali
Format:	Government Document Electronic 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.

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Call Number:	NAS 1.15:2012-217607
NAS 1.15:2012-217607	Available