LEADER 01005cam--2200325---450- 001 990002427340203316 005 20160719093855.0 035 $a000242734 035 $aUSA01000242734 035 $a(ALEPH)000242734USA01 035 $a000242734 100 $a20050601d1976----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $aaf||||||001yy 200 1 $aCompendiario sugli acquedotti pugliesi e lucani$fVincenzo Caruso 210 $aPalo del Colle$cLiantonio$d1976 215 $a653 p., [34] carte di tav.$cill.$d30 cm 606 0 $aAcquedotti$yBasilicata [e] Puglia 676 $a628.15094575 700 1$aCARUSO,$bVincenzo$f<1960- >$0507159 801 0$aIT$bsalbc$gISBD 912 $a990002427340203316 951 $aIII.1. 1817(II 2 7)$bDSSS$cIII.1.$d390326 959 $aBK 969 $aUMA 979 $aDSSS1$b10$c20050601$lUSA01$h1605 979 $aANNAMARIA$b90$c20160719$lUSA01$h0938 996 $aCompendiario sugli acquedotti pugliesi e lucani$9778084 997 $aUNISA LEADER 01966nam 2200493I 450 001 9910703782303321 005 20150526162452.0 035 $a(CKB)5470000002433895 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