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035   $a(EXLCZ)995470000002383800
100   $a20100618d2009      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWindage power loss in gas foil bearings and the rotor-stator clearance of high speed generators operating in high pressure environments$b[electronic resource] /$fRobert J. Bruckner ; prepared for the ASME Turbo Expo 2009 sponsored by ASME, Orlando, Florida, June 8-12, 2009
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2009]
215   $a1 online resource (8 pages) $cillustrations
225 1 $aNASA TM- ;$v2009-215826
300   $aTitle from title screen (viewed on June 17, 2010).
300   $a"November 2009."
300   $a"GT2009-60118."
320   $aIncludes bibliographical references (pages 7-8).
410  0$aNASA technical memorandum ;$v2009-215826.
606   $aFoil bearings$2nasat
606   $aBrayton cycle$2nasat
606   $aClosed cycles$2nasat
606   $aTurbomachinery$2nasat
606   $aHigh pressure$2nasat
606   $aPressure measurement$2nasat
606   $aRotors$2nasat
606   $aShafts (machine elements)$2nasat
615  7$aFoil bearings.
615  7$aBrayton cycle.
615  7$aClosed cycles.
615  7$aTurbomachinery.
615  7$aHigh pressure.
615  7$aPressure measurement.
615  7$aRotors.
615  7$aShafts (machine elements)
700   $aBruckner$b Robert J$01394729
712 02$aNASA Glenn Research Center.
712 12$aASME Turbo Expo$f(2009 :$eOrlando, Fla.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910696909603321
996   $aWindage power loss in gas foil bearings and the rotor-stator clearance of high speed generators operating in high pressure environments$93546203
997   $aUNINA