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R. de Borst, S. Kyriakides and T.J. van Baten (Editors), Stability & Vibration in Thin-Walled Structures, Special Issue of International Journal of Non-Linear Mechanics, Vol. 37, Nos. 4-5, pp 571-1002, June 2002

TABLE OF CONTENTS:
Page 573: Editorial by Rene de Borst, Stelios Kyriakides, Tom van Baten (Editors)
577-588: Haim Abramovich, Josef Singer, Tanchum Weller, Repeated buckling and its influence on the geometrical imperfections of stiffened cylindrical shells under combined loading
589-604: Walter Wunderlich, Ursula Albertin, Buckling behaviour of imperfect spherical shells
605-621: Uwe Hornung, Helmut Saal, Buckling loads of tank shells with imperfections
623-643: Mark W. Hilburger, James H. Starnes, Effects of imperfections on the buckling response of compression-loaded composite shells
645-657: L. Wullschleger, H.-R. Meyer-Piening, Buckling of geometrically imperfect cylindrical shells — definition of a buckling load
659-667: D.H. van Campen, V.P. Bouwman, G.Q. Zhang, J. Zhang, B.J.W. der Weeme, Semi-analytical stability analysis of doubly-curved orthotropic shallow panels — considering the effects of boundary conditions
669-686: H. Öry, H.-G. Reimerdes, T. Schmid, A. Rittweger, J. Gómez Garcı́a, Imperfection sensitivity of an orthotropic spherical shell under external pressure
687-698: V.A. Zarutsky, Investigation of ribs influence on stability and vibration of imperfect shells
699-707: Bodo Geier, A method to compute Koiter's b-factor of anisotropic panels
709-722: Antoine Legay, Alain Combescure, Efficient algorithms for parametric non-linear instability analysis
423-744: Michael P. Nemeth, Richard D. Young, Timothy J. Collins, James H. Starnes, Effects of initial geometric imperfections on the non-linear response of the Space Shuttle superlightweight liquid-oxygen tank
745-756: S. Barlag, H. Rothert, An idealization concept for the stability analysis of ring-reinforced cylindrical shells under external pressure
757-762: Gabriel Cederbaum, David Touati, Postbuckling analysis of imperfect non-linear viscoelastic cylindrical panels
763-775: Zenon Waszczyszyn, Marek Bartczak, Neural prediction of buckling loads of cylindrical shells with geometrical imperfections
777-784: Eugeniusz Bielewicz, Jarosław Górski, Shells with random geometric imperfections simulation — based approach
785-800: Giuseppe Ricciardi, Isaac Elishakoff, A novel local stochastic linearization method via two extremum entropy principles
801-831: David Bushnell, Global optimum design of externally pressurized isogrid stiffened cylindrical shells with added T-rings
833-849: Norman F. Knight, Charles C. Rankin, Frank A. Brogan, STAGS computational procedure for progressive failure analysis of laminated composite structures
851-867: M. Di Sciuva, M. Gherlone, L. Librescu, Implications of damaged interfaces and of other non-classical effects on the load carrying capacity of multilayered composite shallow shells
869-895: V.S Sokolinsky, Y Frostig, S.R Nutt, Special behavior of unidirectional sandwich panels with transversely flexible core under statical loading
897-908: Eduard Riks, Charles C. Rankin, Sandwich modeling with an application to the residual strength analysis of a damaged compression panel
909-920: Jian-Xue Xu, Hong Huang, Pei-Zhen Zhang, Ji-Qing Zhou, Dynamic stability of shallow arch with elastic supports—application in the dynamic stability analysis of inner winding of transformer during short circuit
921-935: A.H. Heinen, J. Büllesbach, On the influence of geometric imperfections on the stability and vibration of thin-walled shell structures
937-949: E.L. Jansen, Non-stationary flexural vibration behaviour of a cylindrical shell
951-966: Carlo Sansour, Werner Wagner, Peter Wriggers, Jamal Sansour, An energy–momentum integration scheme and enhanced strain finite elements for the non-linear dynamics of shells
967-986: Peretz P. Friedmann, Kuo-An Yuan, Marino de Terlizzi, An aeroelastic model for composite rotor blades with straight and swept tips. Part I: Aeroelastic stability in hover
987-1002: R.J. Zwaan, B.B. Prananta, Fluid/structure interaction in numerical aeroelastic simulation

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