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The Effect of Secondary Flows on the Starting Pressure for a Second-throat Supersonic Ejector
The effect of the secondary flow on the starting pressure of a second-throat supersonic ejector has been investigated by adapting the height of the secondary flow inlet. The obtained results show that an optimum value of the secondary inlet height exists, and the starting pressure of the ejector bec...
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Published in: | Journal of thermal science 2011-12, Vol.20 (6), p.503-509 |
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container_title | Journal of thermal science |
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creator | Chen, Jian Wu, Jiping Wang, Zhenguo Luo, Wenlei |
description | The effect of the secondary flow on the starting pressure of a second-throat supersonic ejector has been investigated by adapting the height of the secondary flow inlet. The obtained results show that an optimum value of the secondary inlet height exists, and the starting pressure of the ejector becomes a minimum at that condition. Based on the results of the pressure measurements, a qualitative analysis has been made to clarify the flow behavior and the physical meaning of the performance diagram. It appears that the choking phenomenon of the secondary flow plays an important role in the starting process of the ejector. When the secondary inlet height is relatively small, the choked secondary flow and the supersonic primary flow could be employed to protect the static pressure in the suction chamber from being disturbed by the back pressure effect at a certain primary stagnation pressure, which is lower than the starting pressure for the case of the zero-secondary flow. However, as the secondary inlet height increases and exceeds a critical value, the static pressure in the suction chamber rapidly increases, and the starting pressure of the ejector increases accordingly. |
doi_str_mv | 10.1007/s11630-011-0502-5 |
format | article |
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The obtained results show that an optimum value of the secondary inlet height exists, and the starting pressure of the ejector becomes a minimum at that condition. Based on the results of the pressure measurements, a qualitative analysis has been made to clarify the flow behavior and the physical meaning of the performance diagram. It appears that the choking phenomenon of the secondary flow plays an important role in the starting process of the ejector. When the secondary inlet height is relatively small, the choked secondary flow and the supersonic primary flow could be employed to protect the static pressure in the suction chamber from being disturbed by the back pressure effect at a certain primary stagnation pressure, which is lower than the starting pressure for the case of the zero-secondary flow. 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Therm. Sci</addtitle><addtitle>Journal of Thermal Science</addtitle><description>The effect of the secondary flow on the starting pressure of a second-throat supersonic ejector has been investigated by adapting the height of the secondary flow inlet. The obtained results show that an optimum value of the secondary inlet height exists, and the starting pressure of the ejector becomes a minimum at that condition. Based on the results of the pressure measurements, a qualitative analysis has been made to clarify the flow behavior and the physical meaning of the performance diagram. It appears that the choking phenomenon of the secondary flow plays an important role in the starting process of the ejector. When the secondary inlet height is relatively small, the choked secondary flow and the supersonic primary flow could be employed to protect the static pressure in the suction chamber from being disturbed by the back pressure effect at a certain primary stagnation pressure, which is lower than the starting pressure for the case of the zero-secondary flow. However, as the secondary inlet height increases and exceeds a critical value, the static pressure in the suction chamber rapidly increases, and the starting pressure of the ejector increases accordingly.</description><subject>Classical and Continuum Physics</subject><subject>Engineering Fluid Dynamics</subject><subject>Engineering Thermodynamics</subject><subject>Heat and Mass Transfer</subject><subject>Physics</subject><subject>Physics and Astronomy</subject><subject>二次流</subject><subject>启动压力</subject><subject>喉道</subject><subject>喷射压力</subject><subject>喷射器</subject><subject>超音速</subject><subject>进气口</subject><subject>静态压力</subject><issn>1003-2169</issn><issn>1993-033X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><recordid>eNp9UNtKQzEQDKJgrX6Ab_EDopuTk6TnUUprhYJCK_giIc2lF2pSkxTx701p8VFY2IWd2dkZhG4p3FMA-ZApFQwIUEqAQ0P4GerRrmMEGHs_rzMAIw0V3SW6ynkDIKRgbQ99zFcOj7x3puDo8cyZGKxOP3i8jd8Zx4BLBcyKTmUdlvg1uZz3yWEfE9YnOCmrFHXBs_3OpRzD2uDRph6M6RpdeL3N7ubU--htPJoPJ2T68vQ8fJwSw2hbiBFeLKwZNNpz3oDtjHaGglmAqCttHVjvZCu7lgt-KCe4lNZSayQ01Vkf0eNdk2LOyXm1S-vPakNRUId81DEfVfNRh3wUr5zmyMkVG5YuqU3cp1Df_Jd0dxJaxbD8qrw_JdYNZMtgwH4BTRx0Wg</recordid><startdate>20111201</startdate><enddate>20111201</enddate><creator>Chen, Jian</creator><creator>Wu, Jiping</creator><creator>Wang, Zhenguo</creator><creator>Luo, Wenlei</creator><general>SP Science Press</general><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>~WA</scope><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20111201</creationdate><title>The Effect of Secondary Flows on the Starting Pressure for a Second-throat Supersonic Ejector</title><author>Chen, Jian ; Wu, Jiping ; Wang, Zhenguo ; Luo, Wenlei</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c314t-c6f6bdc82af5520d9caec10cb06c6fade0dfe747945655655e6577dd1dc702003</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2011</creationdate><topic>Classical and Continuum Physics</topic><topic>Engineering Fluid Dynamics</topic><topic>Engineering Thermodynamics</topic><topic>Heat and Mass Transfer</topic><topic>Physics</topic><topic>Physics and Astronomy</topic><topic>二次流</topic><topic>启动压力</topic><topic>喉道</topic><topic>喷射压力</topic><topic>喷射器</topic><topic>超音速</topic><topic>进气口</topic><topic>静态压力</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chen, Jian</creatorcontrib><creatorcontrib>Wu, Jiping</creatorcontrib><creatorcontrib>Wang, Zhenguo</creatorcontrib><creatorcontrib>Luo, Wenlei</creatorcontrib><collection>维普_期刊</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>中文科技期刊数据库-7.0平台</collection><collection>中文科技期刊数据库- 镜像站点</collection><collection>CrossRef</collection><jtitle>Journal of thermal science</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chen, Jian</au><au>Wu, Jiping</au><au>Wang, Zhenguo</au><au>Luo, Wenlei</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>The Effect of Secondary Flows on the Starting Pressure for a Second-throat Supersonic Ejector</atitle><jtitle>Journal of thermal science</jtitle><stitle>J. Therm. Sci</stitle><addtitle>Journal of Thermal Science</addtitle><date>2011-12-01</date><risdate>2011</risdate><volume>20</volume><issue>6</issue><spage>503</spage><epage>509</epage><pages>503-509</pages><issn>1003-2169</issn><eissn>1993-033X</eissn><abstract>The effect of the secondary flow on the starting pressure of a second-throat supersonic ejector has been investigated by adapting the height of the secondary flow inlet. The obtained results show that an optimum value of the secondary inlet height exists, and the starting pressure of the ejector becomes a minimum at that condition. Based on the results of the pressure measurements, a qualitative analysis has been made to clarify the flow behavior and the physical meaning of the performance diagram. It appears that the choking phenomenon of the secondary flow plays an important role in the starting process of the ejector. When the secondary inlet height is relatively small, the choked secondary flow and the supersonic primary flow could be employed to protect the static pressure in the suction chamber from being disturbed by the back pressure effect at a certain primary stagnation pressure, which is lower than the starting pressure for the case of the zero-secondary flow. However, as the secondary inlet height increases and exceeds a critical value, the static pressure in the suction chamber rapidly increases, and the starting pressure of the ejector increases accordingly.</abstract><cop>Heidelberg</cop><pub>SP Science Press</pub><doi>10.1007/s11630-011-0502-5</doi><tpages>7</tpages></addata></record> |
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source | Springer Nature |
subjects | Classical and Continuum Physics Engineering Fluid Dynamics Engineering Thermodynamics Heat and Mass Transfer Physics Physics and Astronomy 二次流 启动压力 喉道 喷射压力 喷射器 超音速 进气口 静态压力 |
title | The Effect of Secondary Flows on the Starting Pressure for a Second-throat Supersonic Ejector |
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