LEADER 01920oam 2200541I 450 001 9910715198003321 005 20201204124902.0 035 $a(CKB)5470000002508029 035 $a(OCoLC)761278868 035 $a(EXLCZ)995470000002508029 100 $a20111115j196809 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 13$aAn experimental and analytical vibration study of thin cylindrical shells with and without longitudinal stiffeners /$fby John L. Sewall and Eugene C. Naumann 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968. 215 $a1 online resource (54 pages) $cillustrations 225 1 $aNASA technical note ;$vTN D-4705 300 $a"September 1968." 320 $aIncludes bibliographical references (pages 28-29). 606 $aCylinders$xVibration 606 $aShells (Engineering)$xTesting 606 $aAluminum alloys$xTesting 606 $aAluminum alloys$xTesting$2fast 606 $aCylinders$xVibration$2fast 606 $aShells (Engineering)$xTesting$2fast 615 0$aCylinders$xVibration. 615 0$aShells (Engineering)$xTesting. 615 0$aAluminum alloys$xTesting. 615 7$aAluminum alloys$xTesting. 615 7$aCylinders$xVibration. 615 7$aShells (Engineering)$xTesting. 700 $aSewall$b John L.$01388451 702 $aNaumann$b Eugene C. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCO 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910715198003321 996 $aAn experimental and analytical vibration study of thin cylindrical shells with and without longitudinal stiffeners$93439050 997 $aUNINA