Integrated turbine tip clearance and gas turbine engine simulation / Jeffryes W. Chapman [and three others]

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Bibliographic Details
Online Access:	Online Access
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.

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Call Number:	NAS 1.15:2016-219146
NAS 1.15:2016-219146	Available