LEADER 01893nam  2200481   450 
001 9910702487003321
005 20130129155528.0
035   $a(CKB)5470000002427295
035   $a(OCoLC)825822671
035   $a(EXLCZ)995470000002427295
100   $a20130129d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aParticle trajectory and icing analysis of the Eł turbofan engine using LEWICE3D version 3 /$fColin S. Bidwell
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (30 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217696
300   $aTitle from title screen (viewed on Jan. 28, 2013).
300   $a"September 2012."
300   $a"Prepared for the International Conference on Aircraft and Engine Icing and Ground Deicing sponsored by the SAE International, Chicago, Illinois, June 13-17, 2011."
320   $aIncludes bibliographical references (page 8).
606   $aIce formation$2nasat
606   $aTrajectory analysis$2nasat
606   $aMoisture content$2nasat
606   $aParticle trajectories$2nasat
606   $aTurbofan engines$2nasat
615  7$aIce formation.
615  7$aTrajectory analysis.
615  7$aMoisture content.
615  7$aParticle trajectories.
615  7$aTurbofan engines.
700   $aBidwell$b Colin S.$01388649
712 02$aNASA Glenn Research Center,
712 12$aInternational Conference on Aircraft and Engine Icing and Ground Deicing$f(2011 :$eChicago, Ill.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702487003321
996   $aParticle trajectory and icing analysis of the Eł turbofan engine using LEWICE3D version 3$93526869
997   $aUNINA