2005
DOI: 10.1201/9781420058291
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Mechanics of Composite Materials

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Cited by 603 publications
(523 citation statements)
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“…1 Structure of articular cartilage for both cellular and collagen fiber arrangement diagram of in the zones of articular [36] where E f , G f and m f are elastic modulus, shear modulu,s and Poisson's ratio of collagen fiber and E m , G m and m m are elastic modulus, shear modulus, and Poisson's ratio of proteoglycan matrix, respectively. Moreover, V fz represents collagen fibers volume fraction in the deep zone (all in z axis direction) [18][19][20].…”
Section: Mechanical Properties Of Deep Zonementioning
confidence: 99%
See 1 more Smart Citation
“…1 Structure of articular cartilage for both cellular and collagen fiber arrangement diagram of in the zones of articular [36] where E f , G f and m f are elastic modulus, shear modulu,s and Poisson's ratio of collagen fiber and E m , G m and m m are elastic modulus, shear modulus, and Poisson's ratio of proteoglycan matrix, respectively. Moreover, V fz represents collagen fibers volume fraction in the deep zone (all in z axis direction) [18][19][20].…”
Section: Mechanical Properties Of Deep Zonementioning
confidence: 99%
“…3 and 4. To determinate the effective elastic modulus, shear modulus and Poisson's ratio perpendicular to the fiber plane (E z , G zr & m zr ), the modified three dimensional unidirectional micromechanics rule of mixture was used [18][19][20].…”
Section: Mechanical Properties Of the Superficial Zonementioning
confidence: 99%
“…Using the constituent properties (Table 1), fiber volume fractions, and sample dimensions, the fibers and matrix of each ply are homogenized using standard strength of materials methods to obtain effective properties (Kaw, 2006). The sample geometry and a representative volume element are depicted in Figure 6.…”
Section: Ideal Intact Compositementioning
confidence: 99%
“…An effective CTE for each ply is determined following similar strength of materials homogenization methods as previously employed (Kaw, 2006). The longitudinal CTE for each ply is:…”
Section: Composite With Cracksmentioning
confidence: 99%
“…The main reasons for the application of composite structures are low cost, high strength and simple manufacturing process. Unfortunately, there are drawbacks or limitations to use fibre composites [14]. The advantages and disadvantages of mechanical behaviour of composite materials are widely described in many publications [3,13,15,18,33].…”
Section: Introductionmentioning
confidence: 99%