کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
6973079 1453268 2016 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Cook-off test and numerical simulation of AP/HTPB composite solid propellant
موضوعات مرتبط
مهندسی و علوم پایه مهندسی شیمی بهداشت و امنیت شیمی
پیش نمایش صفحه اول مقاله
Cook-off test and numerical simulation of AP/HTPB composite solid propellant
چکیده انگلیسی
A small-scale experimental apparatus is designed to study the cook-off characteristics of AP/HTPB propellant. Then a cook-off model is established according to the apparatus, and compared with the experimental results. The theoretical calculation results are in good agreement with the experimental data. On this basis, the numerical predictions of cook-off properties of a solid rocket motor are performed at different heat fluxes.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Journal of Loss Prevention in the Process Industries - Volume 40, March 2016, Pages 1-9
نویسندگان
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