کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1719597 1520217 2016 10 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Influence study of flow separation on the nozzle vibration response
ترجمه فارسی عنوان
مطالعه اثر جدایش جریان بر واکنش ارتعاشات نازل
کلمات کلیدی
موتور راکتی سوخت جامد؛ جریان جدایی؛ واکنش نوسان. تجزیه و تحلیل طیف. نازل موتور تست
موضوعات مرتبط
مهندسی و علوم پایه مهندسی انرژی مهندسی انرژی و فناوری های برق
چکیده انگلیسی

In the present paper, the vibration response difference of the upper stage nozzle with higher expansion ratio between ground and altitude simulation hot-firing test is analyzed. It indicates that the acceleration response of the nozzle under ground hot-firing test is much higher than that of the altitude condition. In order to find the essential reason, the experimental and numerical simulation studies of the flow separation are developed by using the test engine nozzle. The experimental data show that the nozzle internal flow occurred flow separation and the divergence cone internal wall pressure pulsation increased significantly downstream from the separation location. The numerical simulation and experimental results indicate that the increase of internal wall pressure and turbulence pulsating pressure are the substantial reason of vibration response increasing aggravatingly during the ground firing test.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Propulsion and Power Research - Volume 5, Issue 2, June 2016, Pages 108–117
نویسندگان
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