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Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor
The rotating detonation engine is a propulsion system that obtains thrust using continuously existing detonation waves. A rotating detonation combustor usually has an annular shape that allows detonation waves to propagate in the circumferential direction. In this study, we used a disk-shaped rotati...
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Published in: | Journal of propulsion and power 2017-01, Vol.33 (1), p.80-88 |
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container_title | Journal of propulsion and power |
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creator | Nakagami, Soma Matsuoka, Ken Kasahara, Jiro Kumazawa, Yoshiki Fujii, Jumpei Matsuo, Akiko Funaki, Ikkoh |
description | The rotating detonation engine is a propulsion system that obtains thrust using continuously existing detonation waves. A rotating detonation combustor usually has an annular shape that allows detonation waves to propagate in the circumferential direction. In this study, we used a disk-shaped rotating detonation combustor with a combustion chamber with flat-plane glass walls to observe the structure of the phenomena. Self-luminescence, shadowgraphs, and schlieren visualization experiments were performed and compared. Results revealed that detonation waves were propagating in a mixture layer of three gases, fuel, oxidizer, and burned gas at 1600 to 900 m/s; Chapman-Jouguet velocity was 2376 m/s. Waves maintained a three-dimensional complicated wave shape in the disk-shaped combustion chamber with parallel-jet injectors. |
doi_str_mv | 10.2514/1.B36084 |
format | article |
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A rotating detonation combustor usually has an annular shape that allows detonation waves to propagate in the circumferential direction. In this study, we used a disk-shaped rotating detonation combustor with a combustion chamber with flat-plane glass walls to observe the structure of the phenomena. Self-luminescence, shadowgraphs, and schlieren visualization experiments were performed and compared. Results revealed that detonation waves were propagating in a mixture layer of three gases, fuel, oxidizer, and burned gas at 1600 to 900 m/s; Chapman-Jouguet velocity was 2376 m/s. 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All requests for copying and permission to reprint should be submitted to CCC at ; employ the ISSN (print) or (online) to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2016 by Nagoya University. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0748-4658 (print) or 1533-3876 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><rights>Copyright © 2016 by Nagoya University. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0748-4658 (print) or 1533-3876 (online) to initiate your request. 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A rotating detonation combustor usually has an annular shape that allows detonation waves to propagate in the circumferential direction. In this study, we used a disk-shaped rotating detonation combustor with a combustion chamber with flat-plane glass walls to observe the structure of the phenomena. Self-luminescence, shadowgraphs, and schlieren visualization experiments were performed and compared. Results revealed that detonation waves were propagating in a mixture layer of three gases, fuel, oxidizer, and burned gas at 1600 to 900 m/s; Chapman-Jouguet velocity was 2376 m/s. Waves maintained a three-dimensional complicated wave shape in the disk-shaped combustion chamber with parallel-jet injectors.</description><subject>Combustion</subject><subject>Combustion chambers</subject><subject>Detonation</subject><subject>Detonation waves</subject><subject>Oxidizers</subject><subject>Oxidizing agents</subject><subject>Propulsion</subject><subject>Propulsion systems</subject><subject>Rotating disks</subject><subject>Rotation</subject><subject>Shadowgraph photography</subject><subject>Visualization</subject><subject>Wave propagation</subject><issn>0748-4658</issn><issn>1533-3876</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp9kVtr3DAQhUVoIdtNID9BUAp5carR3Y_pJr3AQqCbtI9mbMtZJ15rI8mh7a-PggsNeejTwMzHmZlzCDkBdsYVyI9w9kloZuUBWYASohDW6DdkwYy0hdTKHpJ3Md4xBtpqsyDN5a-9C_3OjQkH-qOPEw79H0y9H6nvaNo6uklhatIU3HPju095ON7SC5f8OHM_8dFF2o8U6UUf74vNFveupSu_q6eYfDgibzscojv-W5fk5vPl9eprsb768m11vi5QKp2KVoga2pK3KNpSNoY1IPKEO6GNs3WHxsqGG4WG1ZoBdAaUgfysFhxRlWJJTmfdffAPk4up2vWxccOAo_NTrMBaCcB5yTP6_hV656cw5usqLkuhtMl6_6PA6uyyMAr-rW2CjzG4rtpnQzH8roBVz5lUUM2ZZPTDjGKP-ELsNfcElgaHnw</recordid><startdate>201701</startdate><enddate>201701</enddate><creator>Nakagami, Soma</creator><creator>Matsuoka, Ken</creator><creator>Kasahara, Jiro</creator><creator>Kumazawa, Yoshiki</creator><creator>Fujii, Jumpei</creator><creator>Matsuo, Akiko</creator><creator>Funaki, Ikkoh</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>201701</creationdate><title>Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor</title><author>Nakagami, Soma ; Matsuoka, Ken ; Kasahara, Jiro ; Kumazawa, Yoshiki ; Fujii, Jumpei ; Matsuo, Akiko ; Funaki, Ikkoh</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a456t-d33b1d92da3d94c70c13a452e367e8bfa784c275a70b6011f71571360632aa593</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Combustion</topic><topic>Combustion chambers</topic><topic>Detonation</topic><topic>Detonation waves</topic><topic>Oxidizers</topic><topic>Oxidizing agents</topic><topic>Propulsion</topic><topic>Propulsion systems</topic><topic>Rotating disks</topic><topic>Rotation</topic><topic>Shadowgraph photography</topic><topic>Visualization</topic><topic>Wave propagation</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Nakagami, Soma</creatorcontrib><creatorcontrib>Matsuoka, Ken</creatorcontrib><creatorcontrib>Kasahara, Jiro</creatorcontrib><creatorcontrib>Kumazawa, Yoshiki</creatorcontrib><creatorcontrib>Fujii, Jumpei</creatorcontrib><creatorcontrib>Matsuo, Akiko</creatorcontrib><creatorcontrib>Funaki, Ikkoh</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of propulsion and power</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Nakagami, Soma</au><au>Matsuoka, Ken</au><au>Kasahara, Jiro</au><au>Kumazawa, Yoshiki</au><au>Fujii, Jumpei</au><au>Matsuo, Akiko</au><au>Funaki, Ikkoh</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor</atitle><jtitle>Journal of propulsion and power</jtitle><date>2017-01</date><risdate>2017</risdate><volume>33</volume><issue>1</issue><spage>80</spage><epage>88</epage><pages>80-88</pages><issn>0748-4658</issn><eissn>1533-3876</eissn><coden>JPPOEL</coden><abstract>The rotating detonation engine is a propulsion system that obtains thrust using continuously existing detonation waves. A rotating detonation combustor usually has an annular shape that allows detonation waves to propagate in the circumferential direction. In this study, we used a disk-shaped rotating detonation combustor with a combustion chamber with flat-plane glass walls to observe the structure of the phenomena. Self-luminescence, shadowgraphs, and schlieren visualization experiments were performed and compared. Results revealed that detonation waves were propagating in a mixture layer of three gases, fuel, oxidizer, and burned gas at 1600 to 900 m/s; Chapman-Jouguet velocity was 2376 m/s. Waves maintained a three-dimensional complicated wave shape in the disk-shaped combustion chamber with parallel-jet injectors.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.B36084</doi><tpages>9</tpages></addata></record> |
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subjects | Combustion Combustion chambers Detonation Detonation waves Oxidizers Oxidizing agents Propulsion Propulsion systems Rotating disks Rotation Shadowgraph photography Visualization Wave propagation |
title | Experimental Visualization of the Structure of Rotating Detonation Waves in a Disk-Shaped Combustor |
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