Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades /

Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades /

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Bibliographic Details
Main Authors: Ibrahim , Mounir (Author), Gupta, Abhinav (Author), Shyam, Vikram (Author)
Corporate Author: Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format: Government Document Electronic eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2014.
Series:NASA technical memorandum ; 2014-218494.
Subjects:
Computational fluid dynamics.
Turbine blades.
Rotor blades (turbomachinery)
Hole distribution (mechanics)
Hole geometry (mechanics)
Online Access:CONNECT
Description
Item Description:Title from title screen (viewed Aug. 7, 2015).
"November 2014."
"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
Physical Description:1 online resource (19 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 19).

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