Interlaminar shear stresses in solid composite beams using a complete out-of-plane shear deformation model

Computers and Structures

Volumn 66, Issue 6, 1998, Pages 713-723

  Rand, Omri ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL GEOMETRY; COMPUTER SIMULATION; FINITE DIFFERENCE METHOD; FUNCTIONS; LAMINATED COMPOSITES; MATHEMATICAL MODELS; SHEAR DEFORMATION; SHEAR STRESS; STRUCTURAL LOADS; THREE DIMENSIONAL;

CROSS SECTIONAL GEOMETRY; INTERLAMINAR SHEAR STRESS; OUT OF PLANE WARPING;

COMPOSITE BEAMS AND GIRDERS;

EID: 0032020979     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7949(97)00127-2     Document Type: Article

References (25)

1. Ambartsumyan, S. A., Theory of Anisotropic Shells. NASA TT F-118, May 1964.
2. Ochao, O. O. and Reddy, J. N., Finite Element Analysis of Composite Laminates. Kluwer Academic Publisher Inc., The Netherlands, 1992.
3. Noor, A. K. and Burton, W. S., Assessment of shear deformation theories for multilayered composite plates, Appl. Mech. Rev., 1989, 42(1), pp. 1-13.
4. Nosier, A. and Reddy, J. N. On vibration and buckling of symmetric laminated plates according to shear deformation theories. Acta Mechanica, 1992, 94, 123-169.
5. Sankar, B. V. A beam theory for laminated composites and application to torsion problems. Journal of Applied Mechanics, 1993, 60(1), 246-249.
6. Maiti, D. K. and Sinha, P. K. Bending and free vibration analysis of shear deformable laminated composite beams by finite element methods. Journal of Composite Structures, 1994, 29(1), 421-431.
7. Perngjin, F. P. and Nayfeh, A. H. A fully nonlinear theory of curved and twisted composite rotor blades accounting for warping and three-dimensional stress effects. Int. J. Solid Structures, 1994, 31(9), 1309-1340.
8. Reddy, J. N., A Review of Refined Theories of Laminated Composite Plates, Shock Vib. Dig., 22, pp. 3-17, 1990.
9. Robbins, D. H. Jr. and Reddy, J. N., Modeling of Thick Composites Using a Lyerwise Laminate Theory, International Journal for Numerical Methods in Engineering, Vol. 36, pp. 665-677, 1993.
10. Bull, J. W. ed., Numerical Analysis and Modelling of Composite Materials, Analysis of Composite Rotor Blades. Chapman & Hall, London, December 1995, Chap. 1.
11. Giavotto, V., Borri, M., Mantegazza, P., Ghiringhelli, G., Carmaschi, V., Maffioli, G. C. and Mussi, F. Anisotropic beam theory and applications. Computers and Structures, 1983, 16, 402-413.
12. Stemple, A. D. and Lee, S. W. A finite element modeling for composite beams undergoing large deflections with arbitrary cross sectional warping. International Journal of Numerical Methods in Engineering, 1989, 28(9), 2143-2163.
13. Bauchau, O. A. and Liu, S. P. Finite element based modal analysis of helicopter rotor blades. Vertica, 1989, 13(2), 197-206.
14. Berdichevsky, E. A., Armanios, E. and Ashraf, B. Theory of anisotropic thin-walled closed-cross-section beams. Composite Engineering, 1992, 2(5-7), 411-432.
15. Librescu, L. and Song, O., Behavior of Thin-Walled Beams made of Advanced Composite Materials and Incorporating Non-Classical Effects. Appl. Mech. Rev., Nov. 1991, 44(11), Part 2, pp. 5174-5180.
16. Kosmatka, J. B. On the behavior of pretwisted beams with irregular cross-sections. Journal of Applied Mechanics, 1988, 59, 146-152.
17. Song, O. and Librescu, L., Free-Vibration of Composite Rotating Helicopter Blades Modelled as Thin-Walled Beams, Proceeding of the American Society for Composites, University Park, Pennsylvania, October 13-15, 1992.
18. Sankar, B. V. A beam theory for laminated composites and application to torsion problems. Journal of Applied Mechanics, 1993, 60(1), 246-249.
19. Yuan, K., Friedmann, P. P. and Venkatesan, C., Aeroelastic Behavior of Composite Rotor Blades with Swept Tips, 48th Annual Forum of the American Helicopter Society, Washington, D.C., June 3-5, 1992.
20. Kim, T. and Dugundji, J. Nonlinear large amplitude vibration of composite helicopter blade at large static deflection. AIAA Journal, 1993, 31(5), 938-946.
21. Laulusa, A., Nonlinear Composite Beam Model - An Application to the Aeroelasticity of Rotor, 20th European Rotorcraft Forum, Amsterdam, The Netherlands, 4-7 October 1994.
22. Wang, S. S. and Choi, I. Boundary-layer effects in composite laminates: Part 1 - Free edge stress singularities. Journal of Applied Mechanics, 1982, 49(1), 541-548.
23. Wang, S. S. and Choi, I. Boundary-layer effects in composite laminates: Part 2 - Free edge stress solutions and basic characteristics. Journal of Applied Mechanics, 1982, 49(1), 549-560.
24. Rand, O. Nonlinear analysis of orthotropic beams of solid cross-sections. Journal of Composite Structures, 1994, 29(1), 27-45.
25. Rand, O. and Barkai, S. M., A Refined Nonlinear Analysis of Pre-twisted Composite Blades. Journal of Composite Structures, Vol. 39, No. 1-2, pp. 39-54, 1997.