LEADER 01348nam a2200277 i 4500 001 991003895529707536 008 201015m19601961it a b 000 0 ita d 035 $ab14405180-39ule_inst 040 $aBibl. Dip.le Aggr. Matematica e Fisica - Sez. Fisica$beng 082 04$a530.151 084 $aLC QC20 100 1 $aSommerfeld, Arnold,$d1868-1951$0719139 245 10$aLezioni di fisica teorica /$cArnold Sommerfeld 260 $aFirenze :$bSansoni Ed. Scientifiche,$c1960-1961 300 $a6 v. ;$c24 cm 500 $aIncludes index 500 $aTraduzione eseguita sulla 4. ed. tedesca: Wiesbaden, 1949 505 1 $av. 1. Meccanica.--v. 2. Meccanica dei mezzi deformabili.--v. 3. Elettrodinamica.--v. 4. Ottica.--v. 5. Termodinamica e statistica.--v. 6. Equazioni a derivate parziali della Fisica 650 4$aTheoretical physics 907 $a.b14405180$b17-01-21$c21-10-20 912 $a991003895529707536 945 $aLE006 Fondo Polezzo 369$cVol. 1$cEx libris Stefano Polezzo$g1$i2006000185875$lle006$og$pE26.80$q-$rl$s- $t0$u0$v0$w0$x0$y.i15948274$z16-01-21 945 $aLE006 Fondo Polezzo 507$cEx libris Stefano Polezzo$g1$i2006000185882$lle006$og$pE26.80$q-$rl$s- $t0$u0$v0$w0$x0$y.i15949679$z17-01-21 996 $aLezioni di fisica teorica$91769528 997 $aUNISALENTO 998 $ale006$b15-10-20$cm$da $e-$fita$git $h0$i0 LEADER 02133oam 2200649 450 001 9910716002203321 005 20210908085149.0 035 $a(CKB)5470000002518088 035 $a(OCoLC)761105758 035 $a(OCoLC)995470000002518088 035 $a(EXLCZ)995470000002518088 100 $a20111115j197012 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aTheoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges /$fby Sidney C. Dixon, Robert Miserentino, and M. Latrelle Hudson 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1970. 215 $a1 online resource (32 pages) $cillustrations 225 1 $aNASA/TN ;$vD-7003 300 $a"December 1970." 320 $aIncludes bibliographical references (page 15). 606 $aAerodynamic loads$2nasat 606 $aBuckling$2nasat 606 $aConical shells$2nasat 606 $aShells (Engineering) 606 $aAerodynamic load$2fast 606 $aBuckling (Mechanics)$2fast 606 $aShells (Engineering)$2fast 615 7$aAerodynamic loads. 615 7$aBuckling. 615 7$aConical shells. 615 0$aShells (Engineering) 615 7$aAerodynamic load. 615 7$aBuckling (Mechanics) 615 7$aShells (Engineering) 700 $aDixon$b Sidney C.$01406307 702 $aMiserentino$b Robert 702 $aHudson$b M. Latrelle 712 02$aUnited States.$bNational Aeronautics and Space Administration, 712 02$aLangley Research Center. 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910716002203321 996 $aTheoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges$93484910 997 $aUNINA