Experimental Study on Spray Characteristics of Gas-Centered Swirl Coaxial Injectors
Gas-centered swirl coaxial injectors have become an important subject of study for staged combustion rocket engines with hydrocarbon fuels. While these injectors are employed successfully in rocket engines, it is very rare to find the related research results as applicable to design data. An experim...
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Veröffentlicht in: | Journal of fluids engineering 2011-12, Vol.133 (12) |
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creator | Jeon, Jaehyoung Hong, Moongeun Han, Yeoung-Min Lee, Soo Yong |
description | Gas-centered swirl coaxial injectors have become an important subject of study for staged combustion rocket engines with hydrocarbon fuels. While these injectors are employed successfully in rocket engines, it is very rare to find the related research results as applicable to design data. An experimental study on spray characteristics of gas-centered swirl coaxial injectors has been performed. The effects of momentum flux ratio and recess length on the spray characteristics have been investigated by cold flow tests with a photographic technique. The liquid intact length L, which profoundly affects the global spray characteristics, decreases as the momentum flux ratio M increases. The critical momentum flux ratio Mc is introduced to identify the flow patterns as internal or external mixing in the injectors. Concerning the effect of the recess length lR, it is shown that the spray cone angle and the drop size decrease as lR increases. |
doi_str_mv | 10.1115/1.4005344 |
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While these injectors are employed successfully in rocket engines, it is very rare to find the related research results as applicable to design data. An experimental study on spray characteristics of gas-centered swirl coaxial injectors has been performed. The effects of momentum flux ratio and recess length on the spray characteristics have been investigated by cold flow tests with a photographic technique. The liquid intact length L, which profoundly affects the global spray characteristics, decreases as the momentum flux ratio M increases. The critical momentum flux ratio Mc is introduced to identify the flow patterns as internal or external mixing in the injectors. Concerning the effect of the recess length lR, it is shown that the spray cone angle and the drop size decrease as lR increases.</description><identifier>ISSN: 0098-2202</identifier><identifier>EISSN: 1528-901X</identifier><identifier>DOI: 10.1115/1.4005344</identifier><identifier>CODEN: JFEGA4</identifier><language>eng</language><publisher>New York, NY: ASME</publisher><subject>Applied sciences ; Energy ; Energy. 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Fluids Eng</addtitle><description>Gas-centered swirl coaxial injectors have become an important subject of study for staged combustion rocket engines with hydrocarbon fuels. While these injectors are employed successfully in rocket engines, it is very rare to find the related research results as applicable to design data. An experimental study on spray characteristics of gas-centered swirl coaxial injectors has been performed. The effects of momentum flux ratio and recess length on the spray characteristics have been investigated by cold flow tests with a photographic technique. The liquid intact length L, which profoundly affects the global spray characteristics, decreases as the momentum flux ratio M increases. The critical momentum flux ratio Mc is introduced to identify the flow patterns as internal or external mixing in the injectors. Concerning the effect of the recess length lR, it is shown that the spray cone angle and the drop size decrease as lR increases.</description><subject>Applied sciences</subject><subject>Energy</subject><subject>Energy. Thermal use of fuels</subject><subject>Engines and turbines</subject><subject>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</subject><subject>Exact sciences and technology</subject><subject>Multiphase Flows</subject><issn>0098-2202</issn><issn>1528-901X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><recordid>eNo9kDFPwzAUhC0EEqUwMLN4YWBIeXbs2hlRVEqlSgwBiS16cWyRKk0iOxXNv8eoFdMN77unuyPknsGCMSaf2UIAyFSICzJjkuskA_Z1SWYAmU44B35NbkLYAbA0FXpGitVxsL7Z227ElhbjoZ5o39Fi8DjR_Bs9mjHew9iYQHtH1xiSPMLW25oWP41vad7jsYnmTbezZux9uCVXDttg7846J5-vq4_8Ldm-rzf5yzZBrrIxsUJmFbNQmQqlzgCU0lxL5YQRhrtUwhIVai64trXlonaZMBorZ4zMQNTpnDyd_hrfh-CtK4fYBP1UMij_1ihZeV4jso8ndsBgsHUeO9OEfwOXQi05U5F7OHEY9rbc9QffxQqlkDLGSH8Bex5n5g</recordid><startdate>20111201</startdate><enddate>20111201</enddate><creator>Jeon, Jaehyoung</creator><creator>Hong, Moongeun</creator><creator>Han, Yeoung-Min</creator><creator>Lee, Soo Yong</creator><general>ASME</general><general>American Society of Mechanical Engineers</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20111201</creationdate><title>Experimental Study on Spray Characteristics of Gas-Centered Swirl Coaxial Injectors</title><author>Jeon, Jaehyoung ; Hong, Moongeun ; Han, Yeoung-Min ; Lee, Soo Yong</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a279t-e459b1e0bcba589007782857f4c4c2f3506a7a82428ede24df94c8abfcc5904d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2011</creationdate><topic>Applied sciences</topic><topic>Energy</topic><topic>Energy. Thermal use of fuels</topic><topic>Engines and turbines</topic><topic>Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc</topic><topic>Exact sciences and technology</topic><topic>Multiphase Flows</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Jeon, Jaehyoung</creatorcontrib><creatorcontrib>Hong, Moongeun</creatorcontrib><creatorcontrib>Han, Yeoung-Min</creatorcontrib><creatorcontrib>Lee, Soo Yong</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><jtitle>Journal of fluids engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Jeon, Jaehyoung</au><au>Hong, Moongeun</au><au>Han, Yeoung-Min</au><au>Lee, Soo Yong</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental Study on Spray Characteristics of Gas-Centered Swirl Coaxial Injectors</atitle><jtitle>Journal of fluids engineering</jtitle><stitle>J. Fluids Eng</stitle><date>2011-12-01</date><risdate>2011</risdate><volume>133</volume><issue>12</issue><issn>0098-2202</issn><eissn>1528-901X</eissn><coden>JFEGA4</coden><abstract>Gas-centered swirl coaxial injectors have become an important subject of study for staged combustion rocket engines with hydrocarbon fuels. While these injectors are employed successfully in rocket engines, it is very rare to find the related research results as applicable to design data. An experimental study on spray characteristics of gas-centered swirl coaxial injectors has been performed. The effects of momentum flux ratio and recess length on the spray characteristics have been investigated by cold flow tests with a photographic technique. The liquid intact length L, which profoundly affects the global spray characteristics, decreases as the momentum flux ratio M increases. The critical momentum flux ratio Mc is introduced to identify the flow patterns as internal or external mixing in the injectors. Concerning the effect of the recess length lR, it is shown that the spray cone angle and the drop size decrease as lR increases.</abstract><cop>New York, NY</cop><pub>ASME</pub><doi>10.1115/1.4005344</doi></addata></record> |
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subjects | Applied sciences Energy Energy. Thermal use of fuels Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology Multiphase Flows |
title | Experimental Study on Spray Characteristics of Gas-Centered Swirl Coaxial Injectors |
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