Answer:
Explanation:
a.) To calculate the longitudinal tensile strength of the composite as follows:
[tex]\sigma^*_{cl}=\sigma'_m V_m+\sigma^*_fV_f[/tex]
Here [tex]\sigma'_m [/tex] is the stress in the matrix at fibre failure [tex]V_m[/tex] is the volume of matrix material [tex]\sigma^*_f[/tex] is the tensile strength of the fibre and [tex]V_f[/tex] is the volume of fibre phase.
Substituting 0.55 for [tex]V_m[/tex], 0.45 for [tex]V_f[/tex], 35MPa for [tex]\sigma'_m [/tex], 3600MPa for [tex]\sigma^*_f[/tex].
[tex]\sigma^*_{cl}=(35\times0.55)+(3600\times0.45)\\=19.25+1620\\=1639.25MPa[/tex]
b.) To calculate the modulus of elasticity of the composite as follows:
[tex]E_c=E_mV_m+E_fV_f[/tex]
Here, [tex]E_m[/tex] is the modulus of elasticity of matrix, [tex]V_m[/tex] is the volume of matrix material, [tex]E_f[/tex] is the modulus of elasticity of fibre, and [tex]V_f[/tex] is the volume of fibre material.
Substituting 0.55 for [tex]V_m[/tex], 0.45 for [tex]V_f[/tex], 2.4MPa for [tex]E_m [/tex], 131GPa for [tex]E_f[/tex].
[tex]E_c=(2.4\TIMES0.55)+(131\TIMES0.45)\\=1.32+58.95\\=60.27GPa[/tex]