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Integrated turbine tip clearance and gas turbine engine simulation /

Bibliographic Details
Main Author: Chapman, Jeffryes W. (Author)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2016.
Series:NASA technical memorandum ; 2016-219146.
Subjects:
Blade tips.
Gas turbine engines.
Thermodynamics.
Turbine blades.
Turbocompressors.
Online Access:https://purl.fdlp.gov/GPO/gpo77529
Description
Item Description:"October 2016."
Physical Description:1 online resource (17 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 17).