The thermal diffusivity of carbon fiber reinforced composite materials is d
ependent on fiber. matrix, and porosity volume fractions. Since the carbon
fiber thermal conductivity is much greater than the epoxy resin matrix ther
mal conductivity, thermal diffusivity is a good indicator of the fiber volu
me fraction. In this study. through-the-thickness thermal diffusivity image
s were obtained nondestructively on carbon fiber reinforced composite plate
s, and the values varied from 0.0035 to 0.0062 cm(2)/s. The fiber and poros
ity volume fractions were measured destructively. and their values varied f
rom 56.0 to 70.5% and from 0.9 to 7.2%. respectively. The destructive test
data were used as a standard for comparison of three commonly used transver
se equivalent thermal conductivity models: the Stacked Plate. the mixed flo
w Cylindrical Fiber model, and the Composite Circular Assemblage model. In
these models, a porosity correction is also studied. There was very good ag
reement between the Composite Circular Assemblage and Cylindrical Fiber mod
el when porosity levels were less than 2%. The porosity correction helped t
o reduce the chi-squared value by 24% in the Cylindrical Filament model. Fi
nally, the potential is discussed to image fiber volume fraction nondestruc
tively using the described thermal measurement system.