LEADER 00843nam0-2200289---450- 001 990009390250403321 005 20110704144720.0 035 $a000939025 035 $aFED01000939025 035 $a(Aleph)000939025FED01 035 $a000939025 100 $a20110704d1879----km-y0itay50------ba 101 1 $aita 102 $aIT 105 $aa-------001yy 200 1 $aManuale di anatomia comparata$fpel dott. Carlo Gegenbaur$g1. ed. italiana [...] pel dott. Carlo Emery 210 $aNapoli$cEnrico Detken$d1879 215 $a719 p.$cill.$d24 cm 700 1$aGegenbaur,$bCarl$084575 702 1$aEmery,$bCarlo$f<1848- 1925> 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990009390250403321 952 $aIIIb C 27$b1291$fDMVSF 959 $aDMVSF 996 $aManuale di anatomia comparata$9764211 997 $aUNINA LEADER 01900oam 2200565 450 001 9910713431103321 005 20200430135215.0 035 $a(CKB)5470000002501345 035 $a(OCoLC)1117765928 035 $a(EXLCZ)995470000002501345 100 $a20190909d1923 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aWind tunnel tests of five strut sections in yaw /$fby Edward P. Warner 210 1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1923. 215 $a1 online resource (7 pages, 6 unnumbered pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 167 300 $a"November 1923." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references. 606 $aYawing (Aerodynamics) 606 $aAirplanes$xModels 606 $aStruts (Engineering) 606 $aWind tunnel testing 606 $aAirplanes$xModels$2fast 606 $aStruts (Engineering)$2fast 606 $aWind tunnel testing$2fast 606 $aYawing (Aerodynamics)$2fast 615 0$aYawing (Aerodynamics) 615 0$aAirplanes$xModels. 615 0$aStruts (Engineering) 615 0$aWind tunnel testing. 615 7$aAirplanes$xModels. 615 7$aStruts (Engineering) 615 7$aWind tunnel testing. 615 7$aYawing (Aerodynamics) 700 $aWarner$b Edward Pearson$f1894-1958,$01393953 712 02$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 $a9910713431103321 996 $aWind tunnel tests of five strut sections in yaw$93460049 997 $aUNINA