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001 9910715046103321
005 20201119131252.0
035   $a(CKB)5470000002507544
035   $a(OCoLC)760926395
035   $a(EXLCZ)995470000002507544
100   $a20111114j196809    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOn the prediction of the vibratory behavior of free-free truncated conical shells /$fby Eugene C. Naumann
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968.
215   $a1 online resource (32 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4772
300   $a"September 1968."
320   $aIncludes bibliographical references (page 15).
606   $aCylinders$xVibration
606   $aShells (Engineering)$xTesting
606   $aCylinders$xVibration$2fast
606   $aShells (Engineering)$xTesting$2fast
615  0$aCylinders$xVibration.
615  0$aShells (Engineering)$xTesting.
615  7$aCylinders$xVibration.
615  7$aShells (Engineering)$xTesting.
700   $aNaumann$b Eugene C.$01406308
712 02$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   $a9910715046103321
996   $aOn the prediction of the vibratory behavior of free-free truncated conical shells$93484920
997   $aUNINA