Mathematical Simulation of Nonisothermal Hardening of Polymeric Composite Structures of Rocket and Space Machinery
| Authors: Tarasov V.A., Belyakov Ye.V. | Published: 29.08.2013 |
| Published in issue: #1(82)/2011 | |
| Category: Production Process Procedures and Machines | |
| Keywords: polymeric composite materials, hardening process, kinetic and reologic characteristics | |
The mathematical model of hardening the prepreg based on the carbon fabric and the ENFB binder is presented, which allows one to predict the prepreg parameters such as the hardening degree, the complex viscosity of the system, and the gel-formation temperature. The calculated parameters of the process kinetics and reology obtained on the basis of the developed model agree well with experimental data.
