1 |
Salamon, N.J. (1978), "Interlaminar stresses in a layered composite Laminate in bending", Fibre Sci. Technol., 11(4), 305-317.
DOI
|
2 |
Shariyat, M. (2010), "A generalized high-order global-local plate theory for nonlinear bending and buckling analyses of imperfect sandwich plates subjected to thermo-mechanical loads", Compos. Struct., 92(1), 130-143.
DOI
|
3 |
Tahani, M. (2007), "Analysis of laminated composite beams using layerwise displacement theories", Compos. Struct., 79(4), 535-547.
DOI
|
4 |
Tong, J.W., Xie, M.Y. and Shen, M. (2004), "The interlaminar stresses of symmetric composite laminates", J. Reinf. Plast. Compos., 23(10), 1023-1029.
DOI
|
5 |
Vidal, P. and Polit, O. (2008), "A family of sinus finite elements for the analysis of rectangular laminated beams", Compos. Struct., 84(1), 56-72.
DOI
|
6 |
Vidal, P. and Polit, O. (2009), "A refined sine-based finite element with transverse normal deformation for the analysis of laminated beams under thermo mechanical loads", J. Mech. Mater. Struct., 4(6), 1127-1155.
DOI
|
7 |
Wu, C.P. and Kuo, H.C. (1993), "An interlaminar stress mixed finite element method for the analysis of thick laminated composite plates", Compos. Struct., 24(1), 29-42.
DOI
|
8 |
Wu, H. and Yan, X. (2005), "Interlaminar stress modeling of composite laminates with finite element method", J. Reinf. Plast. Compos., 24(3), 130-143.
|
9 |
Aydogdu, M. (2007), "Thermal buckling analysis of cross-ply laminated composite beams with general boundary conditions", Compos. Sci. Technol., 67(6), 1096-1104.
DOI
ScienceOn
|
10 |
Becker, W., Jin, P.P. and Lindemann, J. (2001), "The free-corner effect in thermally loaded laminates", Compos. Struct., 52(1), 97-102.
DOI
|
11 |
Bhaskar, K. and Kaushik, B. (2004), "Simple and exact series solutions for flexure of orthotropic rectangular plates with any combination of clamped and simply supported edges", Compos. Struct., 63(1), 63-68.
DOI
|
12 |
Gatto, A., Mattioni, F. and Friswell, M.I. (2009), "Experimental investigation of bistable winglets to enhance wing lift takeoff capability", J. Aircraft, 46(2), 647-655.
DOI
|
13 |
Cho, M. and Kim, H.S. (2000), "Iterative free-edge stress analysis of composite laminates under extension, bending, twisting and thermal loadings", Int. J. Solid. Struct., 37(3), 435-459.
DOI
|
14 |
Cho, M. and Oh, J. (2003), "Higher order zig-zag plate theory under thermo-electric-mechanical loads combined", Compos.: Part B, 34(1), 67-82.
|
15 |
Cho, M. and Oh, J. (2004), "Higher order zig-zag theory for fully coupled thermo-electric-mechanical smart composite plates", Int. J. Solid. Struct., 41(5-6), 1331-1356.
DOI
|
16 |
Gayen, D. and Roy, T. (2013), "Hygro-Thermal Effects on Stress Analysis of Tapered Laminated Composite Beam", Int. J. Compos. Mater., 3(3), 46-55.
|
17 |
Hu, E.Z., Soutis, C. and Edge, E.C. (1997), "Interlaminar stresses in composite laminates with Interlaminar stresses in composite a circular hole," Compos. Struct., 37(2), 223-232.
DOI
|
18 |
Kassapoglou, C. (1990), "Determination of Interlaminar Stresses in Composite Laminates under Combined Loads", J. Reinf. Plast. Compos., 9(1), 33-58.
DOI
|
19 |
Kress, G., Roos, R., Barbezat, M., Dransfeld, C. and Ermann, P. (2005), "Model for interlaminar normal stress in singly curved laminates", Compos. Struct., 69(4), 458-469.
DOI
|
20 |
Lee, Y.W. (1994), "Interlaminar stress analysis of composite laminates using a sublaminate/layer model" Int. J. Solid. Struct., 31(11), 1549-1564.
DOI
|
21 |
Lee, C.Y. and Liu, D. (1992), "An interlaminar stress continuity theory for laminated composite analysis", Comput. Struct., 42(1), 69-78.
DOI
|
22 |
Murthy, M.V.V.S., Mahapatra, D.R., Badarinarayana, K. and Gopalakrishnan, S. (2005), "A refined higher order finite element for asymmetric composite beams", Compos. Struct., 67(1), 27-35.
DOI
|
23 |
Matsunaga, H. (2002), "Interlaminar stress analysis of laminated composite beams according to global higher-order deformation theories", Compos. Struct., 55(1), 105-114.
DOI
|
24 |
Matsunaga, H. (2003), "Interlaminar stress analysis of laminated composite and sandwich circular arches subjected to thermal/mechanical loading", Compos. Struct., 60(3), 345-358.
DOI
|
25 |
Matsunaga, H. (2004), "A comparison between 2-D single-layer and 3-D layerwise theories for computing interlaminar stresses of laminated composite and sandwich plates subjected to thermal loadings", Compos. Struct., 64(2), 161-177.
DOI
|
26 |
Oh, J. and Cho, M. (2004), "A finite element based on cubic zig-zag plate theory for the prediction of thermo-electric-mechanical behaviours", Int. J. Solid. Struct., 41(5-6), 1357-1375.
DOI
|
27 |
Pagano, N.J. (1969), "Exact solutions for composite laminates in cylindrical bending", J. Compos. Mater., 3(3), 398-411.
DOI
|
28 |
Plagianakos, T.S. and Saravanos, D.A. (2009), "Higher-order layerwise laminate theory for the prediction of interlaminar shear stresses in thick composite and sandwich composite plates", Compos. Struct., 87(1), 23-35.
DOI
|
29 |
Rand, O. (1998), "Interlaminar shear stresses in solid composite beams using a complete out-of-plane shear deformation model", Compos. Struct., 66(6), 713-723.
DOI
|
30 |
Rolfes, R. and Rohwer, K. (2000), "Integrated thermal and mechanical analysis of composite plates and shells", Compos. Sci. Technol., 60(11), 2097-2106.
DOI
|