A description of the hot-melt prepreg process was developed by couplin
g resin matrix flow at the coating and impregnation zones with heat tr
ansfer considerations. Both bismaleimide (BMI) and epoxy resin systems
were used as matrices, with continuous carbon fiber reinforcement. Fo
r the laboratory scale prepregger utilized in this study, the thicknes
s of the resin film produced in a doctor blade was approximately 63% o
f the blade distance, showing good agreement with experimental data. I
n addition, the measured heat transfer coefficient between prepreg and
atmosphere indicated that surface convective resistance is large comp
ared to the internal conductive resistance and thus the chill plate in
the prepregging operation plays an important role in determining prep
reg quality. By formulating an analytical methodology in terms of the
''Prepreg Flow Number'' (PFN) that combined important operating parame
ters (e.g., temperature, pressure, and production rate), a temperature
-pressure-velocity superposition was confirmed for the prepregging pro
cess. In addition, the model could easily be extended to different sca
les and types of prepregging processes with the aid of dimensionless p
arameters that are quite descriptive of the operating conditions emplo
yed in prepreg manufacturing.