LEADER 00906nam a2200265 i 4500 001 991000344249707536 005 20020509165255.0 008 010704s1990 it ||| | ita 035 $ab11344143-39ule_inst 035 $aPARLA206421$9ExL 040 $aDip.to Filosofia$bita 082 0 $a700.103 100 1 $aRasulo, Pio$0453537 245 10$aSociologia dell'arte di massa /$cPio Rasulo 260 $a[Taranto] :$bNuove proposte,$c1990 300 $a84 p. ;$c21 cm. 440 3$aLe vie dell'estetica 650 4$aArte e società 650 4$aCultura popolare 907 $a.b11344143$b02-04-14$c01-07-02 912 $a991000344249707536 945 $aLE005IF XLV C 16$g1$iLE005IFA-3929$lle005$nn.i. duplicato$o-$pE0.00$q-$rl$s- $t0$u0$v0$w0$x0$y.i1151937x$z01-07-02 996 $aSociologia dell'arte di massa$9814934 997 $aUNISALENTO 998 $ale005$b01-01-01$cm$da $e-$fita$git $h0$i1 LEADER 01895nam 2200493I 450 001 9910702356003321 005 20121226161236.0 035 $a(CKB)5470000002426598 035 $a(OCoLC)822966252 035 $a(EXLCZ)995470000002426598 100 $a20121226d2012 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aLarge Eddy Simulation of a film cooling flow injected from an inclined discrete cylindrical hole into a crossflow with zero-pressure gradient turbulent boundary layer /$fPerry L. Johnson, Vikram Shyam 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012. 215 $a1 online resource (23 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2012-217695 300 $aTitle from title screen (viewed on Dec. 26, 2012). 300 $a"August 2012." 320 $aIncludes bibliographical references (pages 22-23). 606 $aLarge eddy simulation$2nasat 606 $aFilm cooling$2nasat 606 $aPressure gradients$2nasat 606 $aReynolds averaging$2nasat 606 $aTurbulent mixing$2nasat 606 $aTurbulent boundary layer$2nasat 615 7$aLarge eddy simulation. 615 7$aFilm cooling. 615 7$aPressure gradients. 615 7$aReynolds averaging. 615 7$aTurbulent mixing. 615 7$aTurbulent boundary layer. 700 $aJohnson$b Perry L$01390438 701 $aShyam$b Vikram$01390439 712 02$aNASA Glenn Research Center. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910702356003321 996 $aLarge Eddy Simulation of a film cooling flow injected from an inclined discrete cylindrical hole into a crossflow with zero-pressure gradient turbulent boundary layer$93443118 997 $aUNINA