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混合管面积和位置对排气引射器性能的影响
引用本文:王广振,吴寿生,王之珊,魏福清.混合管面积和位置对排气引射器性能的影响[J].推进技术,2000,21(4):20-23.
作者姓名:王广振  吴寿生  王之珊  魏福清
作者单位:北京航空航天大学,机械工程及自动化学院,北京,100083
摘    要:通过对一个轴对称波瓣主喷管与4种不同截面积的圆形混合管、并分别在不同轴向位置时的组合试验,研究了混合管与主喷管截面积之比Am/Ap及轴向间距Lmp对排气引射系统的引射系数、压力损失系数和气动性能综合参数等的影响。结果表明:在试验范围内,Am/Ap增大,系统的引射系数增大、综合氯动性能改善;Lmg增大,4系统的引射系数和压力损失系数也增大。对于不同范围,压力损失系数增加的斜率不同,;总的趋势则是综合

关 键 词:航空发动机  喷管  排气引射系统  气动性能

Effect of mixing tube area and position on performances for lobed ejector
Wang Guangzhen,Wu Shousheng,Wang Zhishan and Wei Fuqing.Effect of mixing tube area and position on performances for lobed ejector[J].Journal of Propulsion Technology,2000,21(4):20-23.
Authors:Wang Guangzhen  Wu Shousheng  Wang Zhishan and Wei Fuqing
Institution:Coll.of Mechanical Engineering and Automatization,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;Coll.of Mechanical Engineering and Automatization,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;Coll.of Mechanical Engineering and Automatization,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;Coll.of Mechanical Engineering and Automatization,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China
Abstract:Experimental research for four mixing tubes with different sectional area and different axial distance for a axisymmetric lobed nozzle was conducted to investigate the effect of area ratio A m/ A p and axial distance L mp between lobed nozzle and mixing tube on the aerodynamic performances for a lobed exhaust system. The results show that the pumping coefficient increase and synthetic aerodynamic performance of the system can be improved with the increase of A m/ A p.The pumping coefficient and pressure loss coefficient of the system also increase with L mp increase.The slope of pressure loss coefficient with L mp change is different in different range, and the synthetic aerodynamic performance be worse with L mp increase.
Keywords:Engine nozzle  Exhaust ejector system  Aerodynamic performance
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