An assessment of gas foil bearing scalability and the potential benefits to civilian turbofan engines /

Bibliographic Details

Main Author:	Bruckner, Robert J.
Corporate Authors:	NASA Glenn Research Center, ASME Turbo Expo
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:	NASA technical memorandum ; 216732.
Subjects:	Foil bearings. Turbomachinery. Lubrication systems. Cooling. Damping. Gas bearings. Shafts (Machine elements) Turbofan engines.
Online Access:	https://purl.fdlp.gov/GPO/gpo3629