LEADER 01146nam 2200325Ia 450 001 996387077903316 005 20221108045659.0 035 $a(CKB)1000000000629111 035 $a(EEBO)2240969730 035 $a(OCoLC)12444997 035 $a(EXLCZ)991000000000629111 100 $a19850830d1690 uy | 101 0 $aeng 135 $aurbn#|||a|bb| 200 10$aHis Majesties most gracious speech to both houses of Parliament, on Tuesday the twenty fifth of November, 1690$b[electronic resource] 210 $aLondon $cPrinted by Charles Bill and Thomas Newcomb ...$d1690 215 $a4 p 300 $aReproduction of original in Huntington Library. 300 $aA request for more military supplies. 330 $aeebo-0113 607 $aGreat Britain$xHistory$yWilliam and Mary, 1689-1702 701 $aWilliam$cKing of England,$f1650-1702.$01000870 801 0$bEAA 801 1$bEAA 801 2$bm/c 801 2$bWaOLN 906 $aBOOK 912 $a996387077903316 996 $aHis Majesties most gracious speech to both houses of Parliament, on Tuesday the twenty fifth of November, 1690$92402560 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