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.
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."
Physical Description:1 online resource (8 pages) : illustrations (some color)
Bibliography:Includes bibliographical references (page 8)

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