LEADER 00714nam0-22002891i-450- 001 990003294990403321 005 20001010 035 $a000329499 035 $aFED01000329499 035 $a(Aleph)000329499FED01 035 $a000329499 100 $a20000920d1909----km-y0itay50------ba 101 0 $aita 105 $ay-------001yy 200 1 $aCORSI D'ACQUA DELLA SICILIA 210 $aRoma$cG. Civelli$d1909 215 $app. 389 610 0 $aSicilia 676 $a021.101 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990003294990403321 952 $a021.101.COR.01$b4646$fDECGE 959 $aDECGE 996 $aCORSI D'ACQUA DELLA SICILIA$9446054 997 $aUNINA DB $aING01 LEADER 02158oam 2200601 450 001 9910716734103321 005 20210825112211.0 035 $a(CKB)5470000002524836 035 $a(OCoLC)1159597686 035 $a(EXLCZ)995470000002524836 100 $a20200623d1938 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$hIII$iMass distributed along the wings /$fby Oscar Seidman and A.I. Neihouse 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938. 215 $a1 online resource (12 pages, 17 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 664 300 $a"September 1938." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 12). 517 3 $aMass distributed along the wings 606 $aAirplanes$xWings 606 $aAirplanes$xTail surfaces 606 $aSpin (Aerodynamics) 606 $aWind tunnel testing 606 $aAirplanes$xTail surfaces$2fast 606 $aAirplanes$xWings$2fast 606 $aSpin (Aerodynamics)$2fast 606 $aWind tunnel testing$2fast 615 0$aAirplanes$xWings. 615 0$aAirplanes$xTail surfaces. 615 0$aSpin (Aerodynamics) 615 0$aWind tunnel testing. 615 7$aAirplanes$xTail surfaces. 615 7$aAirplanes$xWings. 615 7$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$bOCLCO 801 2$bTRAAL 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910716734103321 996 $aFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails$93483584 997 $aUNINA