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[an error occurred while processing this directive]一种小型全轴摆动喷管流场计算和性能分析
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尚永腾(1987-),男,山东德州人,工程师,研究方向:固体火箭发动机喷管设计与研究。 |
收稿日期: 2019-01-17
网络出版日期: 2025-05-19
基金资助
航空基金(20180112001);中国空空导弹研究院科技创新基金(201604S06)
Flow Field Calculation and Performance Analysis of a Small Axisymmetric Swing Nozzle
Received date: 2019-01-17
Online published: 2025-05-19
尚永腾 , 白涛涛 . 一种小型全轴摆动喷管流场计算和性能分析[J]. 弹箭与制导学报, 2019 , 39(4) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2019.04.001
In order to analyze the flow field and performance of a small long-tail axisymmetric swing nozzle, A series of different conditions were calculated by 3-D CFD simulation method. The results show that the swing nozzle has a uniform flow field that nearly invariable with different angle. There are high local pressure and low velocity vortex near the split line which are related to pressure, channel-throat ratio and working medium. The swing nozzle has low thrust lost, high deflecting efficiency and good linearity and the swing brings small inner flow load and great fiction force. The good flow field uniformity and better performance of the swing nozzle is verified and measures to reduce shaking moment are proposed.
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