کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1714522 1013328 2014 32 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Effects of a hot jet on detonation initiation and propagation in supersonic combustible mixtures
ترجمه فارسی عنوان
اثرات یک جت داغ در شروع و انتشار انفجار در مخلوط قابل احتراق فراصوتی
کلمات کلیدی
پالایش توری سازنده، مخلوط قابل احتراق فوق العاده آغاز و انتشار، اثرات جت داغ،
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی
The effects of a hot jet on detonation initiation and propagation in supersonic combustible mixtures has been studied with two-dimensional numerical simulations with the open-source program AMROC that uses a block-structured adaptive mesh refinement method. Results indicate that the hot jet could ignite the detonation effectively in supersonic combustible mixtures like a pneumatic ramp. After the realization of the detonation initiation, the hot jet can still play an important role on the detonation propagation during its continuous ejection. For a hot jet with certain diameter, it can result in an overdriven detonation with almost constant overdrive degree. After the shutdown of the hot jet, the stable CJ detonation combustion was realized finally in the supersonic combustible mixtures. With the re-ejection of the hot jet, the failed detonation could be reinitiated quickly. Through the control of the re-ejection of the hot jet, it plays a key role not only in the initiation process, but also in the subsequent continuous detonation combustion period.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 105, Issue 1, December 2014, Pages 265-277
نویسندگان
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