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  • Base de données et galerie internationale d'ouvrages d'art et du génie civil

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La bibliographie suivante contient toutes les publications répertoriées dans la base de données qui sont reliées à ce nom en tant qu'auteur, éditeur ou collaborateur.

  1. Somers, M. / Weller, T. / Abramovich, H. (1991): Influence of predetermined delaminations on buckling and postbuckling behavior of composite sandwich beams. Dans: Composite Structures, v. 17, n. 4 ( 1991).

    https://doi.org/10.1016/0263-8223(91)90024-s

  2. Somers, M. / Weller, T. / Abramovich, H. (1992): Buckling and postbuckling behavior of delaminated sandwich beams. Dans: Composite Structures, v. 21, n. 4 ( 1992).

    https://doi.org/10.1016/0263-8223(92)90050-m

  3. Abramovich, H. / Livshits, A. (1993): Dynamic behavior of cross-ply laminated beams with piezoelectric layers. Dans: Composite Structures, v. 25, n. 1-4 ( 1993).

    https://doi.org/10.1016/0263-8223(93)90184-r

  4. Abramovich, H. / Grunwald, A. (1995): Stability of axially impacted composite plates. Dans: Composite Structures, v. 32, n. 1-4 ( 1995).

    https://doi.org/10.1016/0263-8223(95)00079-8

  5. Abramovich, H. / Pletner, B. (1997): Actuation and sensing of piezolaminated sandwich type structures. Dans: Composite Structures, v. 38, n. 1-4 ( 1997).

    https://doi.org/10.1016/s0263-8223(97)00037-8

  6. Abramovich, H. / Meyer-Piening, H.-R (1998): Induced vibrations of piezolaminated elastic beams. Dans: Composite Structures, v. 43, n. 1 (septembre 1998).

    https://doi.org/10.1016/s0263-8223(98)00094-4

  7. Abramovich, H. (1998): Deflection control of laminated composite beams with piezoceramic layers — closed form solutions. Dans: Composite Structures, v. 43, n. 3 (novembre 1998).

    https://doi.org/10.1016/s0263-8223(98)00104-4

  8. Rikards, R. / Abramovich, H. / Auzins, J. / Korjakins, A. / Ozolinsh, O. / Kalnins, K. / Green, T. (2004): Surrogate models for optimum design of stiffened composite shells. Dans: Composite Structures, v. 63, n. 2 (février 2004).

    https://doi.org/10.1016/s0263-8223(03)00171-5

  9. Rikards, R. / Abramovich, H. / Kalnins, K. / Auzins, J. (2006): Surrogate modeling in design optimization of stiffened composite shells. Dans: Composite Structures, v. 73, n. 2 (mai 2006).

    https://doi.org/10.1016/j.compstruct.2005.11.046

  10. Gal, E. / Lévy, R. / Abramovich, H. / Pavsner, P. (2006): Buckling analysis of composite panels. Dans: Composite Structures, v. 73, n. 2 (mai 2006).

    https://doi.org/10.1016/j.compstruct.2005.11.052

  11. Abramovich, H. (2011): A new insight on vibrations and buckling of a cantilevered beam under a constant piezoelectric actuation. Dans: Composite Structures, v. 93, n. 2 (janvier 2011).

    https://doi.org/10.1016/j.compstruct.2010.08.013

  12. Pevzner, P. / Abramovich, H. / Weller, T. (2008): Calculation of the collapse load of an axially compressed laminated composite stringer-stiffened curved panel–An engineering approach. Dans: Composite Structures, v. 83, n. 4 (juin 2008).

    https://doi.org/10.1016/j.compstruct.2007.05.001

  13. Rosen, A. / Abramovich, H. (1984): Galerkin method as a tool to investigate the planar and non-planar behavior of curved beams. Dans: Computers & Structures, v. 18, n. 1 (janvier 1984).

    https://doi.org/10.1016/0045-7949(84)90092-0

  14. Abramovich, H. / Weller, T. / Yaffe, R. (1990): Application of a modified donnell technique for the determination of critical loads of imperfect plates. Dans: Computers & Structures, v. 37, n. 4 (janvier 1990).

    https://doi.org/10.1016/0045-7949(90)90036-2

  15. Yaffe, R. / Abramovich, H. (2003): Dynamic buckling of cylindrical stringer stiffened shells. Dans: Computers & Structures, v. 81, n. 8-11 (mai 2003).

    https://doi.org/10.1016/s0045-7949(02)00417-0

  16. Yocum, M. / Abramovich, H. / Grunwald, A. / Mall, S. (2003): Fully reversed electromechanical fatigue behavior of composite laminate with embedded piezoelectric actuator/sensor. Dans: Smart Materials and Structures, v. 12, n. 4 (août 2003).

    https://doi.org/10.1088/0964-1726/12/4/307

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