Abstract
Laminate composites are used widely in diverse fields because of the ubiquitous advantages it provides compared to others. These materials are susceptible to developing of micro cracks which will change the global response of material thus creating high stresses and heightened damage in the other part. To precisely predict its life and practical applications, considering material strength and its capability to resist damage is important. This paper intends in finding out optimum conditions for minimum damage progression. A flat plate with stress concentrations in form of cut-outs made up of Epoxycarbon UD (Prepreg) and [45 0 −45 90]s layup has been modelled; progressive failure analysis under uni-axial tension loading is performed. Comparison of failure criteria is done and ultimately Hashin failure criteria is chosen for static analysis with different layups, cut-out shapes, sizes, orientations and multiple cut-outs. The observations are noted and outcomes are compared.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Hiton MJ, Soden PD (1998) Predicting failure in composite laminates: the background to the exercise. Compos Sci Technol (Impact Factor: 3.63) 58(7):1001–1010. https://doi.org/10.1016/s0266-3538(98)00074-8
Sun CT (2008) Strength analysis of unidirectional composites and laminates. Compr Compos Mater Sci 1:641–666
Icardi U, Locatto S, Longo A (2007) Assessment of recent theories for predicting failure of composite laminates. Appl Mech Rev 60:76–86
Camanho PP, Matthews FL (1999) A progressive damage model for mechanically fastened joints in composite laminates. J Compos Mater 23:2248–2249
Nguyen BN (1997) Three-dimensional modeling of damage in laminated composites containing a central hole. J Compos Mater 31:1672–1693
American Society for Testing and Materials (2006) Standard test method for short beam strength of polymer matrix composite materials and their laminates. ASTM Standard D 2344/D 2344M, ASTM International
Tirkas K, Kortschot MT (1995) The relationship between critical strain energy release rate and delamination Mmde in mutidirectional carbon-fibre/epoxy laminates. ASTM STP 1285:283–304
Hashin Z (1980) Failure criteria for unidirectional fiber composites. J Appl Mech 47:329–334
Lessard LB, Chang FK (1991) Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: part II – experiment. J Compos Mater 25:44–64
Chen WH, Lee SS, Yeh JT (1995) Three-dimensional contact stress analysis of a composite laminate with bolted joint. Compos Struct 30:287–297
Ochoa OO, Reddy JN (1992) Finite element analysis of composite laminates. Kluwer Academic Publishers
Sleight DW. Progressive failure analysis methodology for laminated composite structures, NASA/TP-1999-209107
Chang FK, Lessard LB (1991) Damage tolerance of laminated composite containing an open hole and subjected to compressive loadings: part I – analysis. J Compos Mater 25:2–43
Tserpes KI, Labeas G, Papanikos P, Kermanidis T (2002) Stength prediction of bolted joints in graphite/epoxy composite laminates. Compos: Part B 33:521–529
Venkateshwar Reddy C (2018) J Eng Res Appl 8(7):21–24 (Part -III). www.ijera.com. ISSN 2248-9622
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Switzerland AG
About this paper
Cite this paper
Achanta, Y., Ramesh Babu, P., Sandeep, D. (2020). Progressive Damage Analysis of Laminated Composites. In: Satapathy, S., Raju, K., Molugaram, K., Krishnaiah, A., Tsihrintzis, G. (eds) International Conference on Emerging Trends in Engineering (ICETE). Learning and Analytics in Intelligent Systems, vol 2. Springer, Cham. https://doi.org/10.1007/978-3-030-24314-2_62
Download citation
DOI: https://doi.org/10.1007/978-3-030-24314-2_62
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-24313-5
Online ISBN: 978-3-030-24314-2
eBook Packages: EngineeringEngineering (R0)