02056nam 2200553 a 450 991069995760332120110420085228.0(CKB)5470000002406380(OCoLC)699832518(EXLCZ)99547000000240638020110201d2010 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierAn 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, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (7 pages) illustrationsNASA/TM ;2010-216732Title from title screen (viewed on Feb. 1, 2011)."August 2010.""GT2010-22118."Includes bibliographical references (page 7).Foil bearingsnasatTurbomachinerynasatLubrication systemsnasatCoolingnasatDampingnasatGas bearingsnasatShafts (machine elements)nasatTurbofan enginesnasatFoil bearings.Turbomachinery.Lubrication systems.Cooling.Damping.Gas bearings.Shafts (machine elements)Turbofan engines.Bruckner Robert J1394729NASA Glenn Research Center.ASME Turbo Expo(2010 :Glasgow, Scotland)GPOGPOBOOK9910699957603321An assessment of gas foil bearing scalability and the potential benefits to civilian turbofan engines3510835UNINA