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