Investigation of Effects of Fiber Orientation Angles on Deflection Behavior of Cantilever Laminated Composite Square Plates

Year 2020, Volume: 23 Issue: 3, 633 - 639, 01.09.2020

Savaş Evran

https://doi.org/10.2339/politeknik.558815

Cited By: 4

Abstract

In this study, the deflection response of cantilever
laminated composite square plates subjected to the weight of itself was
analyzed using finite element and Taguchi methods. The plates with 12 plies
were made of glass fiber reinforced polymer composites (GFRP). The arrangements
and fiber orientation angles of the plies were conducted using Taguchi’s L9
(33) orthogonal array. Each four plies was assumed to be control factor. Fiber
orientation angles were varied from 10 to 90 in degree. Plates were modelled
using finite element software ANSYS Parametric Design Language. Analysis of
signal-to-noise (S/N) ratio was used in order to evaluate the control factors
with the optimum levels for minimum deflection response. Analysis of variance
was carried out in order to analyze the powerful influential control factors
and their percent contributions on responses.  

Keywords

Fiber reinforced composite laminates, finite element analysis, Taguchi method, plate

References

• [1] Sayyad A.S. and Ghugal Y.M., "Bending, buckling and free vibration of laminated composite and sandwich beams: A critical review of literature", Composite Structures, 171: 486-504, (2017).
• [2] Rakočević M. and Vatin N., "Bending of Laminated Composite Plates", Applied Mechanics and Materials, 725-726: 667-73, (2015).
• [3] Rakočević M. and Popović S., "Bending analysis of simply supported rectangular laminated composite plates using a new computation method based on analytical solution of layerwise theory", Archive of Applied Mechanics, 88: 671-89, (2018).
• [4] Iyengar N.G.R. and Umaretiya J.R., "Deflection analysis of hybrid laminated composite plates", Composite Structures, 5: 15-32, (1986).
• [5] Reddy B.S., Reddy A.R., Kumar J.S. and Reddy K.V.K., "Bending analysis of laminated composite plates using finite element method", International Journal of Engineering, Science and Technology, 4: 177-90, (2012).
• [6] Ćetković M. and Vuksanović D., "Bending, free vibrations and buckling of laminated composite and sandwich plates using a layerwise displacement model", Composite Structures, 88: 219-27, (2009).
• [7] Maiti D.K. and Sinha P.K., "Bending, free vibration and impact response of thick laminated composite plates", Computers & Structures, 59: 115-29, (1996).
• [8] Karama M., Abou Harb B., Mistou S. and Caperaa S., "Bending, buckling and free vibration of laminated composite with a transverse shear stress continuity model", Composites Part B: Engineering, 29: 223-34, (1998).
• [9] Khdeir A.A. and Reddy J.N., "An exact solution for the bending of thin and thick cross-ply laminated beams", Composite Structures, 37: 195-203, (1997).
• [10] Lee K.H., Lin W.Z. and Chow S.T., "Bidirectional bending of laminated composite plates using an improved zig-zag model", Composite Structures, 28: 283-94, (1994).
• [11] Zhang Y.X. and Yang C.H., "Recent developments in finite element analysis for laminated composite plates", Composite Structures, 88: 147-57, (2009).
• [12] Yam L.H., Wei Z., Cheng L. and Wong W.O., "Numerical analysis of multi-layer composite plates with internal delamination", Computers & Structures, 82: 627-37, (2004).
• [13] MINITAB. Software (Minitab Inc State College, PA, USA) (wwwminitabcom).
• [14] Ross P.J., Taguchi Techniques for Quality Engineering: McGraw-Hill International Editions, 2nd Edition, New York, USA; 1996.
• [15] ANSYS. Software (ANSYS Inc, Canonsburg, PA, USA) (wwwansyscom).
• [16] ANSYS. Help (Version 13).