LEADER 00800nam0-22002771i-450- 001 990006169450403321 005 19980601 035 $a000616945 035 $aFED01000616945 035 $a(Aleph)000616945FED01 035 $a000616945 100 $a19980601d1987----km-y0itay50------ba 105 $a--------00-yy 200 1 $aProfili giuridici della cessione delle partecipazioni statali$fRaffaello Capunzo. 210 $aNapoli$cJovene$d1987 215 $a170 p.$d24 cm 676 $a346.067 700 1$aCapunzo,$bRaffaello$0230951 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990006169450403321 952 $aVI E 206$b24163*$fFGBC 959 $aFGBC 996 $aProfili giuridici della cessione delle partecipazioni statali$9197784 997 $aUNINA DB $aGIU01 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