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LEADER: 01883nam 2200289 a 45 0
001 a191130
008 971020s1988 caua b f000|0 eng d
040 $aCMontNP$cCMontNP
086 0 $aD 208.14/2:NPS-53-88-003
100 1 $aDanielson, D. A.$q(Donald A.).
245 10 $aTripping of stiffened plates using a refined beam theory /$cby Donald Danielson.
260 $aMonterey, Calif. :$bNaval Postgraduate School ;$aSpringfield, Va. :$bAvailable from National Technical Information Service,$c[1988?]
300 $a26 [3] p. :$bill. ;$c28 cm.
500 $aCover title.
500 $a"NPS-53-88-003."
500 $a"Technical report for period October 1987 - March 1988."
500 $aAD A193 941.
504 $aIncludes bibliographical references (p. 23-25).
520 $aThe subject of this paper is the buckling behavior of thin bar stiffeners attached to plates which are subjected to normal pressure loadings. The stiffeners are mathematically modeled by a nonlinear beam theory recently derived. An analytical solution is obtained to the beam buckling equations. The curvature of the centerline along the beam's base at the buckling load is expressed in terms of the beam's thickness, height, and rotational stiffness. Analytical results are compared with an experiment recently performed. Keywords: Tripping, Buckling, Plates, Beams, Stiffeners, Structures, Solid mechanics, Submarines, Ships, Aircraft, Grillages, Bars, Frames, Pressure, Elasticity, Stability, Panel, Compression.
592 $aaq/ /aq cc:9116 10/20/97
650 4 $aSTIFFENING.
650 4 $aBUCKLING.
650 4 $aBEAMS(STRUCTURAL).
710 2 $aNaval Postgraduate School (U.S.).$bDept. of Mathematics
740 01 $aNPS-53-88-003.
926 $aNPS-LIB$bDIGIPROJ$cD 208.14/2:NPS-53-88-003$dBOOK$eNEVER$f1
926 $aNPS-LIB$bFEDDOCS$cD 208.14/2:NPS-53-88-003$dBOOK$f2