[1]
|
A. Jain, C. S. Upadhyay and P. M. Mohite, “Fibre Breaking Damage Model for Unidirectional Fibrous Composites Using Micromechanics,” 16th National Seminar on Aerospace Structures (NASAS), IIT Bombay, 2009.
|
[2]
|
V. Murari, “Micromechanics Based Continuum Damage Model for Ply Failure in Unidirectional Composites,” Ph.D. Thesis, Department of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur Uttar Pradesh, 2010.
|
[3]
|
S. Biswas, “Micromechanics Based Damage Mesomodel for Unidirectional Fibrous Laminated Composite,” M. Tech. Thesis, Department of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur Uttar Pradesh, 2011.
|
[4]
|
ASTM D3379-75, “Standard Test Method for Tensile Strength and Young’s Modulus for High Modulus Single Filament Fibers,” ASTM Standards, 1975.
|
[5]
|
Y. Yamashita, S. Kawabata, S. Okada and A. Tanaka, “Mechanical Characteristics of PBO Single Fiber,” 2003.
www.mat.usp.ac.jp/polymer-composite/253.PDF
|
[6]
|
D. Sinclair, “A Bending Method for Measurement of the Tensile Strength and Young’s Modulus of Glass Fibers,” Journal of Applied Physics, Vol. 21, No. 5, 1950, pp. 380-386. doi:+10.1063/1.1699670
|
[7]
|
“Torayca Carbon Fibres Technical Information,”
http://www.torayca.com/en/index.html
|
[8]
|
I. P. Kumar, “Mechanical and Damage Characterization of Single Carbon and Glass Fibres,” M. Tech. Thesis, Department of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur Uttar Pradesh, 2010, pp.
|
[9]
|
D. Hartman, D. M. Miller and M. E. Greenwood, “High Strength Glass Fibers,” Moving Forward with 50 Years of Leadership in Advanced Materials, Vol. 39, 1994, pp. 415-426.
|
[10]
|
P. D. Soden, M. J. Hinton and A. S. Kaddour, “Lamina Properties, Lay-Up Configurations and Loading Conditions for a Range of Fibre-Reinforced Composite Laminates,” Composite Science and Technology, Vol. 58, No. 7, 1998, pp. 1011-1022.
doi:10.1016/S0266-3538(98)00078-5
|