An assessment of gas foil bearing scalability and the potential benefits to civilian turbofan engines [electronic resource] / Robert J. Bruckner ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers, Glasgow, Scotland, United Kingdom, June 14-18, 2010.

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Bibliographic Details
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Main Author:	Bruckner, Robert J.
Corporate Authors:	NASA Glenn Research Center, ASME Turbo Expo
Format:	Government Document Electronic 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.

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Call Number:	NAS 1.15:2010-216732
NAS 1.15:2010-216732	Available