LEADER 01966nam  2200493I  450 
001 9910703782303321
005 20150526162452.0
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035   $a(OCoLC)910116245
035   $a(EXLCZ)995470000002433895
100   $a20150526j201502    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFundamental study of a single point lean direct injector part I $eeffect of air swirler angle and injector tip location on spray characteristics /$fSarah A. Tedder [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dFebruary 2015.
215   $a1 online resource (14 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218475
300   $aTitle from title screen (viewed on May 26, 2015).
300   $a"February 2015."
300   $a"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, ASEE, Cleveland, Ohio, July 28-30, 2014."
320   $aIncludes bibliographical references (pages 13-14).
517   $aFundamental study of a single point lean direct injector part I 
606   $aTurbulent mixing$2nasat
606   $aTurbulent combustion$2nasat
606   $aFuel injection$2nasat
606   $aRecirculative fluid flow$2nasat
606   $aComputational fluid dynamics$2nasat
615  7$aTurbulent mixing.
615  7$aTurbulent combustion.
615  7$aFuel injection.
615  7$aRecirculative fluid flow.
615  7$aComputational fluid dynamics.
700   $aTedder$b Sarah A.$01393138
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703782303321
996   $aFundamental study of a single point lean direct injector part I$93485103
997   $aUNINA