LEADER 00842nam0-22002771i-450- 001 990005255120403321 005 20090615131909.0 035 $a000525512 035 $aFED01000525512 035 $a(Aleph)000525512FED01 035 $a000525512 100 $a19990604d--------km-y0itay50------ba 101 0 $afre 105 $ay-------001yy 200 1 $aAthènes devant la dèfaite de 404$ehistoire d'une crise idèologique$fpar Edmond Lèvy 210 $aAthènes$cÉcole frantaise d'Athènes et de Rome$dc1976 215 $aIX, 339 p.$d28 cm 676 $a938.505$v22$zita 700 1$aLévy,$bEdmond$0412463 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990005255120403321 952 $a938.5 LEV 1$bANT. G. R. 2681$fFLFBC 959 $aFLFBC 996 $aAthènes devant la dèfaite de 404$9539383 997 $aUNINA 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