LEADER 01996nam  2200493Ia 450 
001 9910699796203321
005 20110126132503.0
035   $a(CKB)5470000002404980
035   $a(OCoLC)698377586
035   $a(EXLCZ)995470000002404980
100   $a20110126d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA data filter for identifying steady-state operating points in engine flight data for condition monitoring applications$b[electronic resource] /$fDonald L. Simon and Jonathan S. Litt ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), 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 (10 pages) $cillustrations
225 1 $aNASA/TM- ;$v2010-216359
300   $aTitle from title screen (viewed on Jan. 26, 2011).
300   $a"July 2010."
300   $a"GT2010-22818."
320   $aIncludes bibliographical references (page 10).
606   $aSteady state$2nasat
606   $aGas turbine engines$2nasat
606   $aFault detection$2nasat
606   $aStructural health monitoring$2nasat
606   $aStatistical analysis$2nasat
615  7$aSteady state.
615  7$aGas turbine engines.
615  7$aFault detection.
615  7$aStructural health monitoring.
615  7$aStatistical analysis.
700   $aSimon$b Donald L$01389758
701   $aLitt$b Jonathan S$01398039
712 02$aNASA Glenn Research Center.
712 12$aASME Turbo Expo$f(2010 :$eGlasgow, Scotland)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699796203321
996   $aA data filter for identifying steady-state operating points in engine flight data for condition monitoring applications$93510814
997   $aUNINA