LEADER 00816nam a2200229 i 4500 001 991001631309707536 008 060517 2004 it ita 020 $a8874021763 035 $ab13402614-39ule_inst 040 $aDip.to Filosofia$bita 082 0 $a149 100 1 $aIannotta, Daniella$0160781 245 13$aLa comunicazione fra simbolo e immagine /$cDaniella Iannotta 260 $aCantalupa :$bEffata,$c2004 300 $a190 p. ;$c21 cm 650 4$aImmagini$xLinguaggio 907 $a.b13402614$b21-09-06$c17-05-06 912 $a991001631309707536 945 $aLE005 149 IAN01. 01$g1$i2005000174667$lle005$o-$pE15.00$q-$rl$s- $t0$u4$v3$w4$x0$y.i14237027$z17-05-06 996 $aComunicazione fra simbolo e immagine$91091594 997 $aUNISALENTO 998 $ale005$b17-05-06$cm$da $e-$fita$git $h3$i0 LEADER 01979oam 2200541 450 001 9910715130103321 005 20201229071716.0 035 $a(CKB)5470000002508715 035 $a(OCoLC)1139565336 035 $a(EXLCZ)995470000002508715 100 $a20200206d1931 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 12$aA comparison of the aerodynamic characteristics of three normal and three reflexed airfoils in the variable density wind tunnel /$fby George L. Defoe 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1931. 215 $a1 online resource (12 pages, 4 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 388 300 $a"August, 1931." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 6). 606 $aAerofoils 606 $aWind tunnel testing 606 $aTrailing edges (Aerodynamics) 606 $aLift (Aerodynamics) 606 $aDrag (Aerodynamics) 606 $aLift (Aerodynamics)$2fast 606 $aTrailing edges (Aerodynamics)$2fast 615 0$aAerofoils. 615 0$aWind tunnel testing. 615 0$aTrailing edges (Aerodynamics) 615 0$aLift (Aerodynamics) 615 0$aDrag (Aerodynamics) 615 7$aLift (Aerodynamics) 615 7$aTrailing edges (Aerodynamics) 700 $aDeFoe$b George L.$01387351 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910715130103321 996 $aA comparison of the aerodynamic characteristics of three normal and three reflexed airfoils in the variable density wind tunnel$93437070 997 $aUNINA