. "3 MATERIALS PROPERTIES AND LIFE PREDICTION." Assessment of Research Needs for Wind Turbine Rotor Materials Technology. Washington, DC: The National Academies Press, 1991.
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Assessment of Research Needs for Wind Turbine Rotor Materials Technology
TABLE 3-2 Typical Properties of Unidirectional Composites
E-Glass/Resin
KEVLAR Resin
Graphite/Resin
S-Glass/Resin
Fiber Direction
Modulus, GPa
44.8
75.8
145
56
Strength tension, MPa
1124
1241
1517
1980
Strength compression, MPa
896
276
2068
626
Coefficient of thermal expansion, microstrain/K
8.8
-4.0
-0.45
5.5
Transverse Direction
Modulus, GPa
11.0
5.52
10.3
11.4
Strength tension, MPa
31
14
48
31
Strength compression, MPa
138
55
138
138
Coefficient of thermal expansion, microstrain/K
22.1
57.6
25.2
23.3
Shear (Inplane)
Modulus, GPa
4.14
2.41
5.52
4.48
Strength, MPa
71.7
34.5
82.7
71.7
Poisson Ratio
Axial-Transverse
0.27
0.34
0.30
0.27
Thickness Direction
Modulus, GPa
11.0
5.5
10.3
11.4
Poisson ratio
0.44
0.38
0.55
0.44
To further illustrate the cost differences based on fibers, consider a hybrid composite with a carbon/glass volume ratio vc/g. The ratio of the cost of the hybrid composite to an all-glass composite to provide the same structural stiffness is given by
The parameters in Equation (1) are defined as follows: $, price per unit mass; s, specific gravity; E, Young's modulus; g, glass; and c, carbon. On the other hand, the weight ratio, defined as the weight of the hybrid composite divided by that of the all-glass composite, is given by
E-glass fiber costs around $2/lb; a high-strength carbon fiber costs about $30/lb. Thus, an all-carbon fiber composite costs 3.5 times more than an all-glass fiber composite to provide the same structural stiffness at a weight savings of 76 percent. When a 50/50 glass/carbon hybrid composite is used, however, the calculated cost ratio is reduced to 2.9 with a weight savings of 58 percent.