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A. Barut

The following bibliography contains all publications indexed in this database that are linked with this name as either author, editor or any other kind of contributor.

  1. Barut, A. / Hanauska, J. / Madenci, E. / Ambur, D. R. (2002): Analysis method for bonded patch repair of a skin with a cutout. In: Composite Structures, v. 55, n. 3 (February 2002).

    https://doi.org/10.1016/s0263-8223(01)00158-1

  2. Kradinov, V. / Hanauska, J. / Barut, A. / Madenci, E. / Ambur, D. R. (2002): Bolted patch repair of composite panels with a cutout. In: Composite Structures, v. 56, n. 4 (June 2002).

    https://doi.org/10.1016/s0263-8223(02)00027-2

  3. Barut, A. / Madenci, E. / Anderson, T. / Tessler, A. (2002): Equivalent single-layer theory for a complete stress field in sandwich panels under arbitrarily distributed loading. In: Composite Structures, v. 58, n. 4 (December 2002).

    https://doi.org/10.1016/s0263-8223(02)00137-x

  4. Madenci, E. / Barut, A. / Phan, N. (2018): Peridynamic unit cell homogenization for thermoelastic properties of heterogenous microstructures with defects. In: Composite Structures, v. 188 (March 2018).

    https://doi.org/10.1016/j.compstruct.2018.01.009

  5. Barut, A. / Madenci, E. / Tessler, A. (2013): C0-continuous triangular plate element for laminated composite and sandwich plates using the {2,2} – Refined Zigzag Theory. In: Composite Structures, v. 106 (December 2013).

    https://doi.org/10.1016/j.compstruct.2013.07.024

  6. Barut, A. / Madenci, E. (2010): A complex potential-variational formulation for thermo-mechanical buckling analysis of flat laminates with an elliptic cutout. In: Composite Structures, v. 92, n. 12 (November 2010).

    https://doi.org/10.1016/j.compstruct.2010.04.013

  7. Barut, A. / Madenci, E. (2009): Analysis of bolted–bonded composite single-lap joints under combined in-plane and transverse loading. In: Composite Structures, v. 88, n. 4 (May 2009).

    https://doi.org/10.1016/j.compstruct.2008.06.003

  8. Barut, A. / Madenci, E. / Tessler, A. / Starnes, J. H. (2000): A new stiffened shell element for geometrically nonlinear analysis of composite laminates. In: Computers & Structures, v. 77, n. 1 (June 2000).

    https://doi.org/10.1016/s0045-7949(99)00201-1

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