LEADER 01911nam  2200505I  450 
001 9910704468803321
005 20130701161042.0
035   $a(CKB)5470000002441005
035   $a(OCoLC)851386633
035   $a(EXLCZ)995470000002441005
100   $a20130701d2012      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn integrated approach for aircraft engine performance estimation and fault diagnostics /$fDonald L. Simon, Jeffrey B. Armstrong
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (13 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2012-217725
300   $aTitle from title screen (viewed on July 1, 2013).
300   $a"October 2012."
300   $a"Prepared for the Turbo Expo 2012 sponsored by the American Society of Mechanical Engineers (ASME) Copenhagen, Denmark, June 11-15, 2012."
300   $a"GT2012-69905."
320   $aIncludes bibliographical references (page 13).
606   $aKalman filters$2nasat
606   $aGas turbine engines$2nasat
606   $aOn-line systems$2nasat
606   $aPerformance prediction$2nasat
606   $aGas path analysis$2nasat
615  7$aKalman filters.
615  7$aGas turbine engines.
615  7$aOn-line systems.
615  7$aPerformance prediction.
615  7$aGas path analysis.
700   $aSimon$b Donald L.$01389758
702   $aArmstrong$b Jeffrey B.
712 02$aNASA Glenn Research Center,
712 12$aASME Turbo Expo$f(2012 :$eCopenhagen, Denmark),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704468803321
996   $aAn integrated approach for aircraft engine performance estimation and fault diagnostics$93464939
997   $aUNINA