Preview

Industrial laboratory. Diagnostics of materials

Advanced search

Determination of the transverse shear stress in layered composites

https://doi.org/10.26896/1028-6861-2020-86-2-44-53

Abstract

An engineering approach to estimation of the transverse shear stresses in layered composites is developed. The technique is based on the well-known D. I. Zhuravsky equation for shear stresses in an isotropic beam upon transverse bending. In general, application of this equation to a composite beam is incorrect due to the heterogeneity of the composite structure. According to the proposed method, at the first stage of its implementation, a transition to the equivalent model of a homogeneous beam is made, for which the Zhuravsky formula is valid. The transition is carried out by changing the shape of the cross section of the beam, provided that the bending stiffness and generalized elastic modulus remain the same. The calculated shear stresses in the equivalent beam are then converted to the stress values in the original composite beam from the equilibrium condition. The main equations and definitions of the method as well as the analytical equation for estimation of the transverse shear stress in a composite beam are presented. The method is verified by comparing the analytical solution and the results of the numerical solution of the problem by finite element method (FEM). It is shown that laminate stacking sequence has a significant impact both on the character and on the value of the transverse shear stress distribution. The limits of the applicability of the developed technique attributed to the conditions of the validity of the hypothesis of straight normal are considered. It is noted that under this hypothesis the shear stresses do not depend on the layer shear modulus, which explains the absence of this parameter in the obtained equation. The classical theory of laminate composites is based on the similar assumptions, which gives ground to use this equation for an approximate estimation of the transverse shear stresses in in a layered composite package.

About the Authors

Yu. I. Dudarkov
N. E. Zhukovsky Central Aerohydrodynamic Institute
Russian Federation

Yuriy I. Dudarkov

1, ul. Zhukovskogo, Zhukovsky, Moscow oblast, 140180



M. V. Limonin
N. E. Zhukovsky Central Aerohydrodynamic Institute
Russian Federation

Mikhail V. Limonin

1, ul. Zhukovskogo, Zhukovsky, Moscow oblast, 140180



References

1. Mikhailov S. E. On the edge effect in layered composites / Mekh. Kompozit. Mater. 1981. N 2. P. 227 – 233 [in Russian].

2. Dudarkov Yu. I., Levchenko E. A., Limonin M. V. Free edge effect in layered composites / Aviats. Promyshl. 2012. N 4. P. 48 – 53 [in Russian].

3. Dudarkov Yu. I., Levchenko E. A., Limonin M. V. Numerical estimation of influence of edge effects on free edges of cut-outs on the strength of laminated composites / Zavod. Lab. Diagn. Mater. 2017. Vol. 83. N 3. P. 59 – 64 [in Russian].

4. Grishin V. I., Dzuba A. S., Dudarkov Yu. I. The strength and buckling of elements and fittings of composite aircraft structures. — Moscow: Fizmatlit, 2013. — 273 p. [in Russian].

5. Baker A., Dutton S., Kelly D. Composite materials for aircraft structures. — Second Edition. — Virginia: American Institute of Aeronautics and Astronautics Inc, 2004. P. 599. DOI: 10.2514/4.861680.

6. Hill R. The mathematical theory of plasticity. — Oxford: Clarendon Press, 1998. P. 355.

7. Tsai S. W. Strength theories of filamentary structures / Schwartz R. T., Schwartz H. S. (Eds.) Fundamental aspects of fiber reinforced plastic composites. — New York: Wiley Interscience, 1968. P. 3 – 11.

8. Tsai S. W., Wu E. M. A General theory of strength for anisotropic materials / Journal of Composite materials. 1971. Vol. 5. P. 58 – 80. DOI: 10.1177/002199837100500106.

9. Hashin Z., Rotem A. A fatigue failure criterion for fiber reinforced materials / Journal of Composite materials. 1973. Vol. 7. P. 448 – 464. DOI: 10.1177/002199837300700404.

10. Hashin Z. Failure criteria for unidirectional fiber composites / Journal of Applied mechanics. 1980. Vol. 47(2). P. 329 – 334. DOI: 10.1115/1.3153664.

11. Puck A., Schurmann H. Failure analysis of FRP laminates by means of physically based phenomenological models / Composites science and technology. 2002. Vol. 62(12 – 13). P. 1633 – 1662. DOI: 10.1016/S0266-3538(01)00208-1.

12. Polilov A. N. Experimental mechanics of composite. — Moscow: MGTU, 2015. — 375 p. [in Russian].

13. Ilichev A. V., Gubin A. M., Akmeev A. R., Ivanov N. V. Definition of aria of the maximum shear deformations for CFRP samples on Iosipescu method, with use of optical system of measurements / Tr. VIAM. 2018. N 6(66). P. 99 – 109. DOI: 10.18577/2307-6046-2018-0-6-99-109 [in Russian].

14. Pagano N. J. Exact Solutions for Composite Laminates in Cylindrical Bending / Journal of Composite Materials. 1969. Vol. 3(1). P. 398 – 411. DOI: 10.1177/002199836900300304.

15. Pagano N. J. Exact Solutions for Rectangular Bidirectional Composites and Sandwich Plates / Journal of Composite Materials. 1970. Vol. 4(1). P. 20 – 34. DOI: 10.1177/002199837000400102.

16. Polilov A. N., Tatus’ N. A. Biomechanics of the strength of layered composites — Moscow: Fizmatlit, 2018. — 328 p. [in Russian].

17. Feodosiev V. I. Strength of materials. — Moscow: Nauka, 1979. — 560 p. [in Russian].


Review

For citations:


Dudarkov Yu.I., Limonin M.V. Determination of the transverse shear stress in layered composites. Industrial laboratory. Diagnostics of materials. 2020;86(2):44-53. (In Russ.) https://doi.org/10.26896/1028-6861-2020-86-2-44-53

Views: 653


ISSN 1028-6861 (Print)
ISSN 2588-0187 (Online)