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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