سال انتشار: ۱۳۸۵
محل انتشار: یازدهمین کنگره ملی مهندسی شیمی ایران
تعداد صفحات: ۱۳
Gheshlaghi – Department of Chemical Engineering, Ferdosi University, Mashhad, Iran
Ghotbi – Department of Chemical Engineering, Sharif University of Technology, Tehran, Iran
Zahedi – Department of Chemical Engineering, Razi University, Kermanshah, Iran, 67149
as a function of time and axial distance. The results were validated by experimental data of a typical rocket motor. Effects of various factors on combustion were evaluated. The proposed model can be easily modified and used for other solid propellants even with low aluminum content.