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001 9910699957603321
005 20110420085228.0
035   $a(CKB)5470000002406380
035   $a(OCoLC)699832518
035   $a(EXLCZ)995470000002406380
100   $a20110201d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn assessment of gas foil bearing scalability and the potential benefits to civilian turbofan engines$b[electronic resource] /$fRobert J. Bruckner ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers, Glasgow, Scotland, United Kingdom, June 14-18, 2010
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (7 pages) $cillustrations
225 1 $aNASA/TM ;$v2010-216732
300   $aTitle from title screen (viewed on Feb. 1, 2011).
300   $a"August 2010."
300   $a"GT2010-22118."
320   $aIncludes bibliographical references (page 7).
606   $aFoil bearings$2nasat
606   $aTurbomachinery$2nasat
606   $aLubrication systems$2nasat
606   $aCooling$2nasat
606   $aDamping$2nasat
606   $aGas bearings$2nasat
606   $aShafts (machine elements)$2nasat
606   $aTurbofan engines$2nasat
615  7$aFoil bearings.
615  7$aTurbomachinery.
615  7$aLubrication systems.
615  7$aCooling.
615  7$aDamping.
615  7$aGas bearings.
615  7$aShafts (machine elements)
615  7$aTurbofan engines.
700   $aBruckner$b Robert J$01394729
712 02$aNASA Glenn Research Center.
712 12$aASME Turbo Expo$f(2010 :$eGlasgow, Scotland)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699957603321
996   $aAn assessment of gas foil bearing scalability and the potential benefits to civilian turbofan engines$93510835
997   $aUNINA