LEADER 01105cam0-22003731i-450- 001 990007892280403321 005 20051116104547.0 035 $a000789228 035 $aFED01000789228 035 $a(Aleph)000789228FED01 035 $a000789228 100 $a20040601g19139999km-y0itay50------ba 101 0 $aita 102 $aIT 105 $aa-------001yy 200 1 $aLezioni sulla scienza delle costruzioni$fCamillo Guidi 205 $a7. ed. 210 $aTorino$cV. Bona$d1913- 215 $av.$d25 cm 327 0 $a1.: Nozioni di statica grafica$a3.: Teoria dell'elelasticità e Resistenza dei materiali$a4.: Teoria dei ponti 610 0 $aStatica grafica 610 0 $aScienza delle costruzioni 676 $a624.177 2 700 1$aGuidi,$bCamillo$f<1853-1941>$0961 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990007892280403321 952 $a13 N 64 27$b14010$fFINBC 952 $a13 M 22 16$b2039$fFINBC 952 $a224-D-18$b2318$fMA1 959 $aFINBC 959 $aMA1 996 $aLezioni sulla scienza delle costruzioni$9123436 997 $aUNINA LEADER 01715oam 2200493 450 001 9910715133803321 005 20201223092008.0 035 $a(CKB)5470000002508678 035 $a(OCoLC)937437961 035 $a(EXLCZ)995470000002508678 100 $a20160208d1931 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 14$aThe pressure distribution over a semicircular wing tip on a biplane in flight /$fby Richard V. Rhode and Eugene E. Lundquist 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1931. 215 $a1 online resource (14 pages, 8 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 379 300 $a"May, 1931." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 4). 606 $aAerodynamic load$xTesting 606 $aBiplanes 606 $aAirplanes$xWings 606 $aAerodynamic load$xTesting$2fast 615 0$aAerodynamic load$xTesting. 615 0$aBiplanes. 615 0$aAirplanes$xWings. 615 7$aAerodynamic load$xTesting. 700 $aRhode$b Richard V.$01386735 702 $aLundquist$b Eugene E. 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bCOP 801 2$bGPO 906 $aBOOK 912 $a9910715133803321 996 $aThe pressure distribution over a semicircular wing tip on a biplane in flight$93545450 997 $aUNINA