Recent research progress on unstart mechanism, detection and control of hypersonic inlet
The present paper aims to provide a summary report on recent research progress about unstart mechanism, detection and control of hypersonic inlet to help the researchers working on hypersonic inlet to further their work. It covers unstart patterns with their mechanisms, monitoring methods for start/...
Gespeichert in:
| Veröffentlicht in: | Progress in aerospace sciences 2017-02, Vol.89, p.1-22 |
|---|---|
| Hauptverfasser: | , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 22 |
|---|---|
| container_issue | |
| container_start_page | 1 |
| container_title | Progress in aerospace sciences |
| container_volume | 89 |
| creator | Chang, Juntao Li, Nan Xu, Kejing Bao, Wen Yu, Daren |
| description | The present paper aims to provide a summary report on recent research progress about unstart mechanism, detection and control of hypersonic inlet to help the researchers working on hypersonic inlet to further their work. It covers unstart patterns with their mechanisms, monitoring methods for start/unstart classification and detection, characterization methods for unstart margin, and methods for unstart suppression and control. At first, the inner mechanisms of various unstart patterns have been surveyed and classified, which are respectively caused by contraction ratio (CR)/internal contraction ratio (ICR), backpressure, Mach number and heat release. Followed, monitoring methods (one is for start/unstart classification and the other is for unstart detection) have been introduced respectively. Thirdly, three types of techniques for margin characterization of unstart are listed, which are respectively based on backpressure, the location of shock train leading edge and pressure distribution. At last, unstart suppression and control have been discussed, which are based on flow control or feedback control. |
| doi_str_mv | 10.1016/j.paerosci.2016.12.001 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_1945719550</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S037604211630080X</els_id><sourcerecordid>1945719550</sourcerecordid><originalsourceid>FETCH-LOGICAL-c340t-6c2b7cda5f8a605730131581e12dd938f9cb3334808c618f554e45e7b2c15e813</originalsourceid><addsrcrecordid>eNqFkFtLAzEQhYMoWKt_QQK-umtms9nNvinFGxQEUfAtpNlZm9Ima5IK_femVJ99Gg5zzlw-Qi6BlcCguVmVo8bgo7FllXUJVckYHJEJyJYX0Fb1MZkw3jYFqys4JWcxrhhjvJNiQj5e0aBLNGBEHcySjsF_ZhGpd3TrYtIh0Q2apXY2bq5pjwlNsrmpXU-Ndyn4NfUDXe5GDNE7a6h1a0zn5GTQ64gXv3VK3h_u32ZPxfzl8Xl2Ny8Mr1kqGlMtWtNrMUjdMNFyBhyEBISq7zsuh84sOOe1ZNI0IAchaqwFtovKgEAJfEquDnPz4V9bjEmt_Da4vFJBV4sWOiFYdjUHl8mgYsBBjcFudNgpYGpPUa3UH0W1p6igUpliDt4egph_-LYYVHagM9jbkEGo3tv_RvwADtl-4w</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1945719550</pqid></control><display><type>article</type><title>Recent research progress on unstart mechanism, detection and control of hypersonic inlet</title><source>ScienceDirect Freedom Collection (Elsevier)</source><creator>Chang, Juntao ; Li, Nan ; Xu, Kejing ; Bao, Wen ; Yu, Daren</creator><creatorcontrib>Chang, Juntao ; Li, Nan ; Xu, Kejing ; Bao, Wen ; Yu, Daren</creatorcontrib><description>The present paper aims to provide a summary report on recent research progress about unstart mechanism, detection and control of hypersonic inlet to help the researchers working on hypersonic inlet to further their work. It covers unstart patterns with their mechanisms, monitoring methods for start/unstart classification and detection, characterization methods for unstart margin, and methods for unstart suppression and control. At first, the inner mechanisms of various unstart patterns have been surveyed and classified, which are respectively caused by contraction ratio (CR)/internal contraction ratio (ICR), backpressure, Mach number and heat release. Followed, monitoring methods (one is for start/unstart classification and the other is for unstart detection) have been introduced respectively. Thirdly, three types of techniques for margin characterization of unstart are listed, which are respectively based on backpressure, the location of shock train leading edge and pressure distribution. At last, unstart suppression and control have been discussed, which are based on flow control or feedback control.</description><identifier>ISSN: 0376-0421</identifier><identifier>EISSN: 1873-1724</identifier><identifier>DOI: 10.1016/j.paerosci.2016.12.001</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Aerodynamics ; Aerospace engineering ; Classification ; Feedback control ; Feedback control systems ; Flow control ; Hypersonic inlets ; Hysteresis characteristics ; Mach number ; Margin characterization ; Monitoring ; Monitoring systems ; Pressure ; Pressure distribution ; Stress concentration ; Unstart (engines) ; Unstart detection and control ; Unstart flow mechanisms</subject><ispartof>Progress in aerospace sciences, 2017-02, Vol.89, p.1-22</ispartof><rights>2016 Elsevier Ltd</rights><rights>Copyright Elsevier BV Feb 2017</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c340t-6c2b7cda5f8a605730131581e12dd938f9cb3334808c618f554e45e7b2c15e813</citedby><cites>FETCH-LOGICAL-c340t-6c2b7cda5f8a605730131581e12dd938f9cb3334808c618f554e45e7b2c15e813</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.paerosci.2016.12.001$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,780,784,3550,27924,27925,45995</link.rule.ids></links><search><creatorcontrib>Chang, Juntao</creatorcontrib><creatorcontrib>Li, Nan</creatorcontrib><creatorcontrib>Xu, Kejing</creatorcontrib><creatorcontrib>Bao, Wen</creatorcontrib><creatorcontrib>Yu, Daren</creatorcontrib><title>Recent research progress on unstart mechanism, detection and control of hypersonic inlet</title><title>Progress in aerospace sciences</title><description>The present paper aims to provide a summary report on recent research progress about unstart mechanism, detection and control of hypersonic inlet to help the researchers working on hypersonic inlet to further their work. It covers unstart patterns with their mechanisms, monitoring methods for start/unstart classification and detection, characterization methods for unstart margin, and methods for unstart suppression and control. At first, the inner mechanisms of various unstart patterns have been surveyed and classified, which are respectively caused by contraction ratio (CR)/internal contraction ratio (ICR), backpressure, Mach number and heat release. Followed, monitoring methods (one is for start/unstart classification and the other is for unstart detection) have been introduced respectively. Thirdly, three types of techniques for margin characterization of unstart are listed, which are respectively based on backpressure, the location of shock train leading edge and pressure distribution. At last, unstart suppression and control have been discussed, which are based on flow control or feedback control.</description><subject>Aerodynamics</subject><subject>Aerospace engineering</subject><subject>Classification</subject><subject>Feedback control</subject><subject>Feedback control systems</subject><subject>Flow control</subject><subject>Hypersonic inlets</subject><subject>Hysteresis characteristics</subject><subject>Mach number</subject><subject>Margin characterization</subject><subject>Monitoring</subject><subject>Monitoring systems</subject><subject>Pressure</subject><subject>Pressure distribution</subject><subject>Stress concentration</subject><subject>Unstart (engines)</subject><subject>Unstart detection and control</subject><subject>Unstart flow mechanisms</subject><issn>0376-0421</issn><issn>1873-1724</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNqFkFtLAzEQhYMoWKt_QQK-umtms9nNvinFGxQEUfAtpNlZm9Ima5IK_femVJ99Gg5zzlw-Qi6BlcCguVmVo8bgo7FllXUJVckYHJEJyJYX0Fb1MZkw3jYFqys4JWcxrhhjvJNiQj5e0aBLNGBEHcySjsF_ZhGpd3TrYtIh0Q2apXY2bq5pjwlNsrmpXU-Ndyn4NfUDXe5GDNE7a6h1a0zn5GTQ64gXv3VK3h_u32ZPxfzl8Xl2Ny8Mr1kqGlMtWtNrMUjdMNFyBhyEBISq7zsuh84sOOe1ZNI0IAchaqwFtovKgEAJfEquDnPz4V9bjEmt_Da4vFJBV4sWOiFYdjUHl8mgYsBBjcFudNgpYGpPUa3UH0W1p6igUpliDt4egph_-LYYVHagM9jbkEGo3tv_RvwADtl-4w</recordid><startdate>201702</startdate><enddate>201702</enddate><creator>Chang, Juntao</creator><creator>Li, Nan</creator><creator>Xu, Kejing</creator><creator>Bao, Wen</creator><creator>Yu, Daren</creator><general>Elsevier Ltd</general><general>Elsevier BV</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>201702</creationdate><title>Recent research progress on unstart mechanism, detection and control of hypersonic inlet</title><author>Chang, Juntao ; Li, Nan ; Xu, Kejing ; Bao, Wen ; Yu, Daren</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c340t-6c2b7cda5f8a605730131581e12dd938f9cb3334808c618f554e45e7b2c15e813</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Aerodynamics</topic><topic>Aerospace engineering</topic><topic>Classification</topic><topic>Feedback control</topic><topic>Feedback control systems</topic><topic>Flow control</topic><topic>Hypersonic inlets</topic><topic>Hysteresis characteristics</topic><topic>Mach number</topic><topic>Margin characterization</topic><topic>Monitoring</topic><topic>Monitoring systems</topic><topic>Pressure</topic><topic>Pressure distribution</topic><topic>Stress concentration</topic><topic>Unstart (engines)</topic><topic>Unstart detection and control</topic><topic>Unstart flow mechanisms</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chang, Juntao</creatorcontrib><creatorcontrib>Li, Nan</creatorcontrib><creatorcontrib>Xu, Kejing</creatorcontrib><creatorcontrib>Bao, Wen</creatorcontrib><creatorcontrib>Yu, Daren</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>Progress in aerospace sciences</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chang, Juntao</au><au>Li, Nan</au><au>Xu, Kejing</au><au>Bao, Wen</au><au>Yu, Daren</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Recent research progress on unstart mechanism, detection and control of hypersonic inlet</atitle><jtitle>Progress in aerospace sciences</jtitle><date>2017-02</date><risdate>2017</risdate><volume>89</volume><spage>1</spage><epage>22</epage><pages>1-22</pages><issn>0376-0421</issn><eissn>1873-1724</eissn><abstract>The present paper aims to provide a summary report on recent research progress about unstart mechanism, detection and control of hypersonic inlet to help the researchers working on hypersonic inlet to further their work. It covers unstart patterns with their mechanisms, monitoring methods for start/unstart classification and detection, characterization methods for unstart margin, and methods for unstart suppression and control. At first, the inner mechanisms of various unstart patterns have been surveyed and classified, which are respectively caused by contraction ratio (CR)/internal contraction ratio (ICR), backpressure, Mach number and heat release. Followed, monitoring methods (one is for start/unstart classification and the other is for unstart detection) have been introduced respectively. Thirdly, three types of techniques for margin characterization of unstart are listed, which are respectively based on backpressure, the location of shock train leading edge and pressure distribution. At last, unstart suppression and control have been discussed, which are based on flow control or feedback control.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.paerosci.2016.12.001</doi><tpages>22</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0376-0421 |
| ispartof | Progress in aerospace sciences, 2017-02, Vol.89, p.1-22 |
| issn | 0376-0421 1873-1724 |
| language | eng |
| recordid | cdi_proquest_journals_1945719550 |
| source | ScienceDirect Freedom Collection (Elsevier) |
| subjects | Aerodynamics Aerospace engineering Classification Feedback control Feedback control systems Flow control Hypersonic inlets Hysteresis characteristics Mach number Margin characterization Monitoring Monitoring systems Pressure Pressure distribution Stress concentration Unstart (engines) Unstart detection and control Unstart flow mechanisms |
| title | Recent research progress on unstart mechanism, detection and control of hypersonic inlet |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-24T06%3A55%3A40IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Recent%20research%20progress%20on%20unstart%20mechanism,%20detection%20and%20control%20of%20hypersonic%20inlet&rft.jtitle=Progress%20in%20aerospace%20sciences&rft.au=Chang,%20Juntao&rft.date=2017-02&rft.volume=89&rft.spage=1&rft.epage=22&rft.pages=1-22&rft.issn=0376-0421&rft.eissn=1873-1724&rft_id=info:doi/10.1016/j.paerosci.2016.12.001&rft_dat=%3Cproquest_cross%3E1945719550%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1945719550&rft_id=info:pmid/&rft_els_id=S037604211630080X&rfr_iscdi=true |