LEADER 01714nam 2200493I 450 001 9910705712103321 005 20170711084334.0 035 $a(CKB)5470000002453290 035 $a(OCoLC)992997868 035 $a(EXLCZ)995470000002453290 100 $a20170707j201704 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aCFD study of NACA 0018 airfoil with flow control /$fChristopher A. Eggert, Christopher L. Rumsey 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2017. 215 $a1 online resource (34 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2017-219602 300 $a"April 2017." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (pages 11-13). 606 $aActive control$2nasat 606 $aAirfoils$2nasat 606 $aFlow distribution$2nasat 606 $aNavier-Stokes equation$2nasat 606 $aReynolds averaging$2nasat 606 $aWind tunnel tests$2nasat 615 7$aActive control. 615 7$aAirfoils. 615 7$aFlow distribution. 615 7$aNavier-Stokes equation. 615 7$aReynolds averaging. 615 7$aWind tunnel tests. 700 $aEggert$b Christopher A.$01414455 702 $aRumsey$b C. L$g(Christopher Lockwood),$f1961- 712 02$aLangley Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910705712103321 996 $aCFD study of NACA 0018 airfoil with flow control$93513750 997 $aUNINA