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Publicité

K. P. Rao

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. Gupta, R. K. / Rao, K. P. (1985): Instability of laminated composite thin-walled open-section beams. Dans: Composite Structures, v. 4, n. 4 ( 1985).

    https://doi.org/10.1016/0263-8223(85)90030-3

  2. Gupta, R. K. / Venkatesh, A. / Rao, K. P. (1985): Finite element analysis of laminated anisotropic thin-walled open-section beams. Dans: Composite Structures, v. 3, n. 1 ( 1985).

    https://doi.org/10.1016/0263-8223(85)90026-1

  3. Rao, K. P. (1987): Shear buckling of corrugated composite panels. Dans: Composite Structures, v. 8, n. 3 ( 1987).

    https://doi.org/10.1016/0263-8223(87)90070-5

  4. Rao, K. P. / Gopalkrishna, H. R. (1992): Optimization of composite cylindrical panels for buckling by ranking. Dans: Composite Structures, v. 21, n. 3 ( 1992).

    https://doi.org/10.1016/0263-8223(92)90013-3

  5. Tripathy, Biswajit / Rao, K. P. (1993): Optimum design for buckling of plain and stiffened composite axisymmetric shell panels/shells. Dans: Composite Structures, v. 25, n. 1-4 ( 1993).

    https://doi.org/10.1016/0263-8223(93)90193-t

  6. Ganapathy, S. / Tripathy, Biswajit / Rao, K. P. (1995): Damage and its growth in laminated composite circular/rectangular plates undergoing large deformations. Dans: Composite Structures, v. 32, n. 1-4 ( 1995).

    https://doi.org/10.1016/0263-8223(95)00046-1

  7. Ganapathy, S. / Rao, K. P. (1997): Interlaminar stresses in laminated composite plates, cylindrical/spherical shell panels damaged by low-velocity impact. Dans: Composite Structures, v. 38, n. 1-4 ( 1997).

    https://doi.org/10.1016/s0263-8223(97)00052-4

  8. Bonde, D. H. / Rao, K. P. (1979): Edge reinforced circular elastic inclusions in cylindrical shells. Dans: Computers & Structures, v. 10, n. 5 (octobre 1979).

    https://doi.org/10.1016/0045-7949(79)90049-x

  9. Bonde, D. H. / Rao, K. P. (1980): Stresses around two equal circular elastic inclusions in a pressurised cylindrical shell. Dans: Computers & Structures, v. 11, n. 4 (avril 1980).

    https://doi.org/10.1016/0045-7949(80)90075-9

  10. Sridhar, C. / Rao, K. P. (1995): Estimation of low-velocity impact damage in laminated composite circular plates using nonlinear finite element analysis. Dans: Computers & Structures, v. 54, n. 6 (mars 1995).

    https://doi.org/10.1016/0045-7949(94)00404-q

  11. Venkatesh, A. / Rao, K. P. (1980): A doubly curved quadrilateral finite element for the analysis of laminated anisotropic thin shells of revolution. Dans: Computers & Structures, v. 12, n. 6 (décembre 1980).

    https://doi.org/10.1016/0045-7949(80)90020-6

  12. Tripathy, B. / Rao, K. P. (1992): Stiffened composite cylindrical panels—Optimum lay-up for buckling by ranking. Dans: Computers & Structures, v. 42, n. 4 (février 1992).

    https://doi.org/10.1016/0045-7949(92)90115-g

  13. Murthy, P. V. Ramana / Rao, K. P. (1984): Finite element analysis of laminated anisotropic beams of bimodulus materials. Dans: Computers & Structures, v. 18, n. 5 (janvier 1984).

    https://doi.org/10.1016/0045-7949(84)90024-5

  14. Bonde, D. H. / Rao, K. P. (1978): Circular elastic inclusions in cylindrical shells. Dans: Computers & Structures, v. 8, n. 3-4 (mai 1978).

    https://doi.org/10.1016/0045-7949(78)90178-5

  15. Venkatesh, A. / Rao, K. P. (1982): A laminated anisotropic curved beam and shell stiffening finite element. Dans: Computers & Structures, v. 15, n. 2 (janvier 1982).

    https://doi.org/10.1016/0045-7949(82)90068-2

  16. Venkatesh, A. / Rao, K. P. (1985): Analysis of laminated shells of revolution with laminated stiffeners using a doubly curved quadrilateral finite element. Dans: Computers & Structures, v. 20, n. 4 (janvier 1985).

    https://doi.org/10.1016/0045-7949(85)90028-8

  17. Sridhar, C. / Rao, K. P. (1995): Large deformation finite element analysis of laminated circular composite plates. Dans: Computers & Structures, v. 54, n. 1 (janvier 1995).

    https://doi.org/10.1016/0045-7949(94)00300-r

  18. Venkatesh, A. / Ramana Murthy, P. V. / Rao, K. P. (1986): Finite element analysis of bimodulus composite stiffened thin shells of revolution. Dans: Computers & Structures, v. 22, n. 1 (janvier 1986).

    https://doi.org/10.1016/0045-7949(86)90080-5

  19. Ganapathy, S. / Rao, K. P. (1998): Failure analysis of laminated composite cylindrical/spherical shell panels subjected to low-velocity impact. Dans: Computers & Structures, v. 68, n. 6 (septembre 1998).

    https://doi.org/10.1016/s0045-7949(98)00080-7

  20. Rao, K. P. / Tripathy, Biswajit (1991): Composite cylindrical panels—optimum lay-up for buckling by ranking. Dans: Computers & Structures, v. 38, n. 2 (janvier 1991).

    https://doi.org/10.1016/0045-7949(91)90098-7

  21. Tripathy, B. / Rao, K. P. (1991): Curved composite beams—optimum lay-up for buckling by ranking. Dans: Computers & Structures, v. 41, n. 1 (janvier 1991).

    https://doi.org/10.1016/0045-7949(91)90157-h

  22. Tripathy, Biswajit / Rao, K. P. (1993): Stiffened composite axisymmetric shells—Optimum lay-up for buckling by ranking. Dans: Computers & Structures, v. 46, n. 2 (janvier 1993).

    https://doi.org/10.1016/0045-7949(93)90194-i

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