Composite Materials and Structures
Historically a predominantly aerospace material, fiber-reinforced and particle-reinforced composites are increasingly used in other industries, for example, automobile, marine transport, buildings and civil infrastructure, sporting goods, medical equipment and prosthetic devices etc. With the increased use of composite materials, there is a tremendous need to develop efficient manufacturing techniques, economical and effective repair techniques, and methods to predict the short and long-term behavior of the composite materials and structures made of these materials under a variety of loading and environmental conditions.
The Center for Advanced Composites (CAC) at the University of Florida is dedicated to advancement of the state of the art in composite material research and structural analysis. Combining a diverse assortment of experimental testing equipment and the latest in computational analysis tools, the Center provides a well-balanced approach to increasing the understanding of composite material mechanics.
Impact Mechanics
Fiber reinforced composites have tremendous strength and stiffness in the plane of the fibers. However their strength and stiffness in a direction perpendicular to the fibers is governed mainly by the matrix properties. Thus composite structures perform poorly under impact loads that occur due to dropped hand tools, runway debris, and hailstone. It is important to understand the threshold impact energy that will cause impact damage and also the residual strength after impact damage has occurred. Further, based on our understanding methods need to be devised to increase the energy threshold for impact damage and the impact damage tolerance.
The Center for Advanced Composites have a variety of impact testing machines such as gas gun and drop tower. Finite element methods and simple analytical methods are used to predict the impact response, damage and residual strength of impacted structures.
Sample Publications
- B.V. Sankar (1996) "Low-Velocity Impact Response and Damage in Composite Materials", Fracture of Composites, E. Armanios, Ed., Transtech Publications, Ltd., Switzerland, pp. 555-582.
Fracture Mechanics
As explained in the previous section delamination is a prevalent damage mode in laminated composite structures. Fracture mechanics principles are used in determining the loads at which an existing delamination will begin to grow and also the rate at which it will grow. The loss of stiffness and strength due to delaminations can also be estimated. Translaminar reinforcements such as stitching and z-pinning are found to be effective in improving the fracture toughness of delaminated composites. We are developing experimental and analytical methods to understand the effects of these reinforcements so that laminates with optimum reinforcements can be designed.
Sample Publications
- B.V. Sankar (1991) "A Finite Element for Modeling Delaminations in Composite Beams", Computers & Structures, 38(2):239-246.
- B.V. Sankar and S. Hu (1991) "Dynamic Delamination Propagation in Composite Beams", Journal of Composite Materials, 25(11), 1414-1426, 1991.
- B.V. Sankar and V. Sonik (1995) "Pointwise Energy Release Rate in Delaminated Plates", AIAA Journal, 33(7):1312-1318.
- S.K. Sharma and B.V. Sankar (1995) "Effects of Through-the-Thickness Stitching on Impact and Interlaminar Fracture Properties of Textile Graphite/Epoxy Laminates", NASA Contractor Report 195042.
- B.V. Sankar and S.M. Dharmapuri (1999) "Analysis of a stitched double cantilever beam", Journal of Composite Materials, 32(24):2203-2225.
- Wallace, B.T., B.V. Sankar and P.G. Ifju (1999) "Delamination suppression in sandwich beams using trans-laminar reinforcements", to appear in the Proceedings of the Aerospace Division, IMECE 1999, American Society of Mechanical Engineers.
Micromechanics
Micromechanics is concerned with the prediction of various properties of a composite material system from the properties of the individual constituents and the interfaces between the various phases. Some of the properties that can be predicted easily are stiffness (elastic constants), coefficient of thermal expansion, thermal conductivities etc. Prediction of strength, fracture toughness and nonlinear material properties pose a great challenge. The methods can range from simple formulas such as rule of mixtures, to sophisticated multiscale modeling and molecular dynamic simulations.
Sample Publications
- R.V. Marrey and B.V. Sankar (1997) "A micromechanical model for textile composite plates", J. Composite Materials, 31(12):1187-1213.
- H. Zhu, B.V. Sankar and R.V. Marrey (1997) "Evaluation of failure criteria for fiber composites using finite element micromechanics", J. Composite Materials, 32(8):766-782.
- B.V. Sankar and R.V. Marrey (1997) "Analytical method for micromechanics of textile composites", Composites Science and Technology, 57(6):703-713.
- R.V. Marrey and B.V. Sankar (1995) "Micromechanical Models for Textile Structural Composites", NASA Contractor Report 198229.
Textile Composites
The textile technology (technology of making cloths) is one of the oldest technology known to human beings. The basic textile processes are: braiding, knitting and weaving. Stitching can also be considered as one of these processes. Using textile processes various yarns such as graphite, glass, Kevlar© can be woven into a variety of types of preforms or cloth structures. Then these preforms can be rigidized by impregnating with matrix materials in a mold and cured to form a composite structure. Textile composites, in general, have higher impact resistance and fracture toughness because of the intertwining nature of the yarns. They can also lower manufacturing costs, as they are amenable to high volume production- unlike the conventional tape laying lamination process. The challenges in textile composites are: reliable prediction of their properties (micromechanics), draping behavior of the preforms in a mold of complex shape, and modeling the resin infiltration and curing processes.
Current research efforts in this area are aimed at developing a robust failure criterion and design tool to predict textile composite strength and provide for optimized designs. This is accomplished primarily through micromechanical modeling utilizing the finite element method.
Sample Publications
- R.L. Karkkainen, B.V. Sankar, " A Direct Micromechanics Method for Analysis of Failure Initiation of Plain Weave Textile Composites," Journal of Composites Science and Technology, 66, p137-150, January 2006.
- R.L. Karkkainen, B.V. Sankar, "A Direct Micromechanical Failure Analysis of Textile Composites," American Society for Composites, 20th Annual Technical Conference, Philadelphia, PA, September 2005.
- R.V. Marrey and B.V. Sankar (1995) "Micromechanical Models for Textile Structural Composites", NASA Contractor Report 198229.
Nanocomposites
A new opportunity for improvement of polymer matrix composites began with the discovery of the carbon nanotube, which led to the development of nanoparticles as reinforcements in composite materials. Due to their extremely small size, the number of defects in each particle is small, resulting in characteristically high strength and modulus. Also, the amount of contact area between particle and matrix potentially creates very strong bonding.
Sandwich Construction
Although sandwich construction has been used for hundreds of years, recent developments in light weight core and adhesives have given a new impetus to the use of sandwich construction in aerospace and marine industry. Many of the problems discussed in the previous sections are relevant to sandwich construction also. One of the major issues in sandwich plates is debonding of the face sheets, which reduces the compressive load carrying capacity. Translaminar reinforcements in the form of pins are being investigated.
Sample Publications
- Wallace, B.T., B.V. Sankar and P.G. Ifju (1999) "Delamination suppression in sandwich beams using trans-laminar reinforcements", to appear in the Proceedings of the Aerospace Division, IMECE 1999, American Society of Mechanical Engineers.
- Avery, J.L. and B.V. Sankar (1999) "Compressive failure of sandwich beams with debonded face-sheets", Journal of Composite Materials (in press)
- Sankar, B.V., M. Narayanan and J.L. Avery, III (1999) "Post-buckling Behavior of Debonded Sandwich Composite Beams Under Compression", Paper No. AIAA-99-1295, AIAA SDM Conference, St. Luis, MO, April 1999.
- Avery, J.L., M. Narayanan and B.V. Sankar (1998) "Compressive failure of debonded sandwich beams", Recent Advances in Mechanics of Aerospace Structures and Materials, Ed. B.V. Sankar, American Society of Mechanical Engineers, New York, NY.
- R. Ferri and B.V. Sankar (1997) "A Comparative Study on the Impact resistance of Composite Laminates and Sandwich Panels", J. Thermoplastic Composite Materials, 10:304-315
- Sankar, B.V. and R. Ferri (1997) "Static indentation and low-velocity impact tests on sandwich panels", in Analysis and Design Issues for Modern Aerospace Vehicles, Ed. G.J. Simitses, AD- Vol. 55, ASME, New York, NY, pp. 485-490.
- A. Ericsson and B.V. Sankar (1992) "Contact Stiffness of Sandwich Plates and Applications to Low-Velocity Impact Problems", Sandwich Constructions 2, Vol. 1 Proceedings of the Second International Conference on Sandwich Constructions, Edited by D. Weissman-Berman and K-A. Olsson, Engineering Materials Advisory Services Ltd., West Midlands, U.K., pp. 139-159.59.