LEADER 01029nam0-2200325---450- 001 990010114480403321 005 20161027164626.0 010 $a978-88-6843-228-7 035 $a001011448 035 $aFED01001011448 035 $a(Aleph)001011448FED01 035 $a001011448 100 $a20161027d2015----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $a--------001yy 200 1 $a<>sociologia in esilio$eGino Germani, l'America Latina e le scienze sociali$fAna Alejandra Germani$gpresentazione di Paolo Marzotto$gprefazione di Torcuato Di Tella 210 $aRoma$cDonzelli$d2015 215 $a240 p.$d21 cm 225 1 $aItaliani dall'esilio 610 0 $aGermani, Gino (sociologo, 1911-1979) 610 0 $aAmerica Latina$aCondizioni economiche e sociali$aSec 20 676 $a301.092$v22$zita 700 1$aGermani,$bAna Alejandra 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990010114480403321 952 $a301.092 GER 1$b3955$fBFS 959 $aBFS 997 $aUNINA LEADER 02562oam 2200733 450 001 9910716734503321 005 20210825104918.0 035 $a(CKB)5470000002524832 035 $a(OCoLC)1159597641 035 $a(EXLCZ)995470000002524832 100 $a20200623d1937 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails$hII$iMass distributed along the fuselage /$fby Oscar Seidman and A.I. Neihouse 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937. 215 $a1 online resource (11 pages, 17 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 630 300 $a"December 1937." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 11). 517 3 $aMass distributed along the fuselage 606 $aSpin (Aerodynamics) 606 $aAirplanes$xFuselage 606 $aAirplanes$xTail surfaces 606 $aAirplanes$xWings 606 $aMass (Physics) 606 $aWind tunnel testing 606 $aAerodynamic load 606 $aAerodynamic load$2fast 606 $aAirplanes$xFuselage$2fast 606 $aAirplanes$xTail surfaces$2fast 606 $aAirplanes$xWings$2fast 606 $aMass (Physics)$2fast 606 $aSpin (Aerodynamics)$2fast 606 $aWind tunnel testing$2fast 615 0$aSpin (Aerodynamics) 615 0$aAirplanes$xFuselage. 615 0$aAirplanes$xTail surfaces. 615 0$aAirplanes$xWings. 615 0$aMass (Physics) 615 0$aWind tunnel testing. 615 0$aAerodynamic load. 615 7$aAerodynamic load. 615 7$aAirplanes$xFuselage. 615 7$aAirplanes$xTail surfaces. 615 7$aAirplanes$xWings. 615 7$aMass (Physics) 615 7$aSpin (Aerodynamics) 615 7$aWind tunnel testing. 700 $aSeidman$b Oscar$01405963 702 $aNeihouse$b A. I. 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 $a9910716734503321 996 $aFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails$93483584 997 $aUNINA