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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.
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700   $aNaumann$b Eugene C.$01406308
712 02$aUnited States.$bNational Aeronautics and Space Administration,
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996   $aOn the prediction of the vibratory behavior of free-free truncated conical shells$93484920
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