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带二次流的多喷管超声速引射器性能实验研究

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吴继平 陈健 王振国

国防科学技术大学航天与材料工程学院,长沙410073

强激光与粒子束
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国际标准刊号:ISSN 1001-4322
国内统一刊号:CN 51-1311

摘  要:

为研究多喷管超声速引射器在有二次流情况下的性能,采用模拟器产生给定总温和总压的模拟二次流,在多喷管超声速引射器实验台上进行了一系列实验。重点考察了多喷管引射器的性能以及一次流总压和喷管安装构型对其性能的影响。实验结果表明:多喷管超声速引射器可保证二次流在设计工况下正常工作;二次流的加入大大减小了一次流的总压损失;较低的一次流总压具有更好的压力匹配性能,但引射增压能力也有所降低;合理的喷管安装构型可同时提高引射增压能力和压力匹配能力。提出了将二次流作为“助推器”,以帮助多喷管引射器在较低工况下实现启动的方案,在不增加系统复杂度的前提下提高了引射器的压力匹配能力。[著者文摘]

High Power Laser and Particle Beams

分 类 号:

TN248.5 O354.3

文献标识码:

A

文章编号:

1001-4322(2007)09-1439-05

相关文章:

参考文献(15篇) 耦合文献(3篇)  主题相关

[参考文献]

Experimental investigation on performance of multi-nozzle supersonic ejector with secondary flow

WU Ji-ping, CHEN Jian, WANG Zhen-guo (College of Aerospace and Materials Engineering, National University of Defense Technology, Changsha 410073, China)

Abstract:

An ejector test facility was established to investigate the performance of a multi-nozzle supersonic ejector with a secondary flow. Using the hot rocket exhaust gases as primary and simulated secondary driving fluids, wall static pressure distributions on the ejector were obtained. Emphases were laid on the reliability of the multi-nozzle ejector and the influence of the primary flow total pressure and nozzle assembling configurations on the performance of the ejector. Experimental results show that the pumping requirement of the simulated secondary flow can be satisfied by using the multi-nozzle supersonic ejector. With the secondary flow joined, the pressure losses can be reduced greatly, which almost corresponds to 15 percents of the primary flow total energy. The lower primary flow total pressure leads to better pressure adaptability, Reasonable ejector assembling configuration means higher pumping capacity as well as better pressure adaptability. The secondary flow can be used as a "booster" to help the multi-nozzle ejector start at much lower operating condition, which improves the pressure adaptability without additional system complexity.[著者文摘]

Key words:

Aero-optics; Supersonic ejector; Secondary flow; Supersonic diffuser; Nozzle

收稿日期: 2007-02-28
修订日期: 2007-07-15

基金资助:

国家863计划项目资助课题

作者简介:

吴继平(1978-),男,博士生,研究领域为超声速引射器和高超声速推进技术;jpwu_nudt@sohu.com。

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