A nth-order shear deformation theory for composite laminates in cylindrical bending

A. S. Sayyad; Y. M. Ghugal

Curved and Layered Structures (2015)

  • Volume: 2, Issue: 1
  • ISSN: 2353-7396

Abstract

top
The present study investigates whether an nthorder shear deformation theory is applicable for the composite laminates in cylindrical bending. The theory satisfies the traction free conditions at top and bottom surfaces of the plate and does not require problem dependent shear correction factor which is normally associated with the first order shear deformation theory. The well-known classical plate theory at (n = 1) and higher order shear deformation theory of Reddy at (n = 3) are the perticular cases of the present theory. The governing equations of equilibrium and boundary conditions are obtained using the principle of virtual work. A simply supported laminated composite plate infinitely long in y-direction is considered for the detail numerical study. A closed form solution for simply supported boundary conditions is obtained using Navier’s technique. The displacements and stresses are obtained for different aspect ratios and modular ratios.

How to cite

top

A. S. Sayyad, and Y. M. Ghugal. "A nth-order shear deformation theory for composite laminates in cylindrical bending." Curved and Layered Structures 2.1 (2015): null. <http://eudml.org/doc/276943>.

@article{A2015,
abstract = {The present study investigates whether an nthorder shear deformation theory is applicable for the composite laminates in cylindrical bending. The theory satisfies the traction free conditions at top and bottom surfaces of the plate and does not require problem dependent shear correction factor which is normally associated with the first order shear deformation theory. The well-known classical plate theory at (n = 1) and higher order shear deformation theory of Reddy at (n = 3) are the perticular cases of the present theory. The governing equations of equilibrium and boundary conditions are obtained using the principle of virtual work. A simply supported laminated composite plate infinitely long in y-direction is considered for the detail numerical study. A closed form solution for simply supported boundary conditions is obtained using Navier’s technique. The displacements and stresses are obtained for different aspect ratios and modular ratios.},
author = {A. S. Sayyad, Y. M. Ghugal},
journal = {Curved and Layered Structures},
keywords = {nth-order shear deformation theory; shear correction factor; traction free conditions; laminated composites; cylindrical bending},
language = {eng},
number = {1},
pages = {null},
title = {A nth-order shear deformation theory for composite laminates in cylindrical bending},
url = {http://eudml.org/doc/276943},
volume = {2},
year = {2015},
}

TY - JOUR
AU - A. S. Sayyad
AU - Y. M. Ghugal
TI - A nth-order shear deformation theory for composite laminates in cylindrical bending
JO - Curved and Layered Structures
PY - 2015
VL - 2
IS - 1
SP - null
AB - The present study investigates whether an nthorder shear deformation theory is applicable for the composite laminates in cylindrical bending. The theory satisfies the traction free conditions at top and bottom surfaces of the plate and does not require problem dependent shear correction factor which is normally associated with the first order shear deformation theory. The well-known classical plate theory at (n = 1) and higher order shear deformation theory of Reddy at (n = 3) are the perticular cases of the present theory. The governing equations of equilibrium and boundary conditions are obtained using the principle of virtual work. A simply supported laminated composite plate infinitely long in y-direction is considered for the detail numerical study. A closed form solution for simply supported boundary conditions is obtained using Navier’s technique. The displacements and stresses are obtained for different aspect ratios and modular ratios.
LA - eng
KW - nth-order shear deformation theory; shear correction factor; traction free conditions; laminated composites; cylindrical bending
UR - http://eudml.org/doc/276943
ER -

References

top
  1. [1] Mindlin R.D., Influence of rotatory inertia and shear on flexural motions of isotropic, elastic plates, ASME J. Appl. Mech., 1951, 18, 31-38. Zbl0044.40101
  2. [2] Reddy J.N., A simple higher order theory for laminated composite plates, ASME J. Appl. Mech., 1984, 51, 745-752. Zbl0549.73062
  3. [3] Touratier M., An eflcient standard plate theory, Int. J. Eng. Sci., 1991, 29, 901-916. [Crossref] Zbl0825.73299
  4. [4] Soldatos K.P., A transverse shear deformation theory for homogeneous monoclinic plates, Acta Mech., 1992, 94, 195-220. [Crossref] Zbl0850.73130
  5. [5] Karama M., Afaq K.S., Mistou S., Mechanical behavior of laminated composite beam by new multi-layered laminated composite structures modelwith transverse shear stress continuity, Int. J. Solids Struct., 2003, 40, 1525-1546. Zbl1087.74579
  6. [6] Akavci S.S., Buckling and free vibration analysis of symmetric and anti-symmetric laminated composite plates on an elastic foundation, J. Reinf. Plast. Compos., 2007, 26, 1907-1919. [WoS][Crossref] 
  7. [7] Pagano N.J., Exact solution for composite laminates in cylindrical bending, J. Compos. Mater., 1969, 3, 398-411. [Crossref] 
  8. [8] Reddy J.N., Mechanics of Laminated Composite Plates, CRC Press, Boca Raton 1997. Zbl0899.73002
  9. [9] Soldatos K.P., Watson P., A method for improving the stress analysis performance of two-dimensional theories for composite laminates, Acta Mech., 1997, 123, 163-186. Zbl0908.73047
  10. [10] Shu X.P., Soldatos K.P., Cylindrical bending of angle-ply laminates subjected to different sets of edge boundary conditions, Int. J. Solids Struct., 2000, 37, 4289-4307. [Crossref] Zbl0974.74017
  11. [11] Jalali S.J., Taheri F., An analytical solution for cross-ply laminates under cylindrical bending based on through-thethickness inextensibility, Part I-static loading, Int. J. Solids Struct., 1998, 35, 1559-1574. Zbl0920.73289
  12. [12] Perel V.Y., Palazotta A.N., Finite element formulation for cylindrical bending of a transversely compressible sandwich plate based on assumed transverse strain, Int. J. Solids Struct., 2001, 38, 5373-5409. [Crossref] Zbl1051.74046
  13. [13] Khdeir A.A., Free and forced vibration of antisymmetric angleply laminated plate strips in cylindrical bending, J. Vib. Control, 2001, 7, 781-801. [Crossref] Zbl1045.74026
  14. [14] Park J., Lee S.Y., A new exponential plate theory for laminated composites under cylindrical bending, Trans. Japan Soc. Aero. Space Sci., 2003, 46, 89-95. 
  15. [15] Chen W.Q., Lee K.Y., State-space approach for statics and dynamics of angle-ply laminated cylindrical panels in cylindrical bending, Int. J. Mech. Sci., 2005, 47, 374-387. [Crossref] Zbl1192.74235
  16. [16] Lu C.F., Huang Z.Y., ChenW.Q., Semi-analytical solutions for free vibration of anisotropic laminated plates in cylindrical bending, J. Sound Vib., 2007, 304, 987-995. [WoS] 
  17. [17] Carrera E., Nonlinear response of asymmetrically laminated plates in cylindrical bending, AIAA J., 1992, 31(7), 1353-1357. 
  18. [18] Ghugal Y.M., Sayyad A.S., Cylindrical bending of thick orthotropic plate using trigonometric shear deformation theory, Int. J. Appl. Math. Mech., 2011, 7(5), 98-116. Zbl06000437
  19. [19] Sayyad A.S., Ghugal Y.M., Naik N.S., Bending analysis of laminated composite and sandwich beams according to refined trigonometric beam theory, Curved Layer. Struct., 2015, 2, 279- 289. 
  20. [20] Natarajan S., Ferreira A.J.M., Xuan H.N., Analysis of cross-ply laminated plates using isogeometric analysis and unified formulation, Curved Layer. Struct., 2014, 1, 1-10. 
  21. [21] Sun L., Harik I.E., Analytical solution to bending of stiffened and continuous antisymmetric laminates, Curved Layer. Struct., 2015, 2, 254-270. 
  22. [22] Carpentieri G., Tornabene F., Ascione A., Fraternali F., An accurate one-dimensional theory for the dynamics of laminated composite curved beams, J. Sound Vib., 2015, 336, 96-105. [WoS] 
  23. [23] Ferreira A.J.M., Viola E., Tornabene F., Fantuzzi N., Zenkour A.M., Analysis of sandwich plates by generalized differential quadrature method, Math. Probl. Eng., 2013, Article ID 964367, 12 pages, 2013. doi:10.1155/2013/964367. [WoS][Crossref] Zbl1299.74113
  24. [24] Carrera E., Filippi M., Zappino E., Free vibration analysis of laminated beam by polynomial, trigonometric, exponential and zigzag theories, J. Compos. Mater., 2014, 48(19), 2299–2316. [WoS][Crossref] 
  25. [25] Tornabene F., 2-D GDQ solution for free vibrations of anisotropic doubly-curved shells and panels of revolution, Compos. Struct., 2011, 93(7), 1854-1876. [Crossref][WoS] 
  26. [26] Tornabene F., Fantuzzi N., Viola E., Carrera E., Static analysis of doubly-curved anisotropic shells and panels using CUF approach, differential geometry and differential quadrature method, Compos. Struct., 2014, 107, 675-697. [WoS] 
  27. [27] Xiang S., Kang G.W., Xing B., A nth-order shear deformation theory for the free vibration analysis on the isotropic plates, Meccanica, 2012, 47, 1913-1921. [Crossref][WoS] Zbl1293.74213
  28. [28] Xiang S., Jiang S., Bi Z., Jin Y., Yang M., A nth-order meshless generalization of Reddy’s third-order shear deformation theory for the free vibration on laminated composite plates, Compos. Struct., 2011, 93, 299-307. 
  29. [29] Xiang S., Kang G.W., A nth-order shear deformation theory for the bending analysis on the functionally graded plates, Eur. J. Mech.: A/Solids, 2013, 37, 336-343. [WoS] 
  30. [30] Xiang S., Kang G.W., Liu Y. A nth-order shear deformation theory for natural frequency of the functionally graded plates on elastic foundation, Compos. Struct., 2014, 111, 224-231. [WoS] 
  31. [31] Sayyad A.S., Ghumare S.M., Sasane S.T., Cylindrical bending of orthotropic plate strip based on nth-order plate theory, J.Mater. Eng. Struct., 2014, 1, 47-57. 

NotesEmbed ?

top

You must be logged in to post comments.

To embed these notes on your page include the following JavaScript code on your page where you want the notes to appear.

Only the controls for the widget will be shown in your chosen language. Notes will be shown in their authored language.

Tells the widget how many notes to show per page. You can cycle through additional notes using the next and previous controls.

    
                

Note: Best practice suggests putting the JavaScript code just before the closing </body> tag.