LEADER 01060nam0-22003491i-450- 001 990003928730403321 005 20130611113021.0 010 $a88-458-0340-6 035 $a000392873 035 $aFED01000392873 035 $a(Aleph)000392873FED01 035 $a000392873 100 $a20030910d2001----km-y0itay50------ba 101 0 $aita 200 1 $a<>nuova indagine sulle cause di morte$ela codifica automatica, il bridge coding e altri elementi innovativi$fIstituto Nazionale di Statistica$ga cura di Luisa Frova 210 $aRoma$cIstat$d2001 215 $a128 p.$d26 cm 225 1 $aMetodi e norme$fIstat$v8 225 1 $aNuova Serie 610 0 $aCause di morte$aBridge coding 676 $a382 702 1$aFrova,$bLuisa 710 01$aIstat$0374421 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990003928730403321 952 $aCDI-MN-08-01-5$b9090$fMAS 952 $a62 31(083.4)MN(NS)/8$fDAGEA 959 $aMAS 959 $aDAGEA 996 $aNuova indagine sulle cause di morte$9511849 997 $aUNINA LEADER 01896oam 2200529 450 001 9910714048703321 005 20201113143306.0 035 $a(CKB)5470000002507160 035 $a(OCoLC)1136490319 035 $a(EXLCZ)995470000002507160 100 $a20200116d1930 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aSpan load distribution on two monoplane wing models as affected by twist and sweepback /$fby Montgomery Knight and Richard W. Noyes 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1930. 215 $a1 online resource (7 pages, 12 unnumbered pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 346 300 $a"July, 1930." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 5). 606 $aAirplanes$xModels$xWings 606 $aLoads (Mechanics) 606 $aStability of airplanes 606 $aAirplanes$xModels$xWings$2fast 606 $aLoads (Mechanics)$2fast 606 $aStability of airplanes$2fast 615 0$aAirplanes$xModels$xWings. 615 0$aLoads (Mechanics) 615 0$aStability of airplanes. 615 7$aAirplanes$xModels$xWings. 615 7$aLoads (Mechanics) 615 7$aStability of airplanes. 700 $aKnight$b Montgomery$01390967 702 $aNoyes$b Richard W. 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 $a9910714048703321 996 $aSpan load distribution on two monoplane wing models as affected by twist and sweepback$93487447 997 $aUNINA