On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2.5
The results of an experimental study of the perturbation development created by pulsed glow discharge on the swept wing surface with periodic distributed roughness along the leading edge at Mach 2.5 are presented. This work continues research on this model at Mach 2. It was found that the mean flow...
Gespeichert in:
| Hauptverfasser: | , , , , |
|---|---|
| Format: | Tagungsbericht |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | 1 |
| container_start_page | |
| container_title | |
| container_volume | 2351 |
| creator | Panina, A. Yatskikh, A. Kosinov, A. Yermolaev, Yu Semionov, N. |
| description | The results of an experimental study of the perturbation development created by pulsed glow discharge on the swept wing surface with periodic distributed roughness along the leading edge at Mach 2.5 are presented. This work continues research on this model at Mach 2. It was found that the mean flow modulation in the boundary layer of a swept wing with a sweep angle of 40 degrees leads to a change in the amplitude of artificial pulsations excited in the boundary layer by a disturbance source and to a strengthening of the oblique breakdown mechanism at a Mach number of 2.5. |
| doi_str_mv | 10.1063/5.0052064 |
| format | Conference Proceeding |
| fullrecord | <record><control><sourceid>proquest_scita</sourceid><recordid>TN_cdi_proquest_journals_2531410000</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2531410000</sourcerecordid><originalsourceid>FETCH-LOGICAL-p2034-1fdf8467826cb2de6951211193a840c79b00e46a40f05669d8abea789e0cdd03</originalsourceid><addsrcrecordid>eNp9kD9PwzAUxC0EEqUw8A0ssSGlPDu2k4yo4p9U1KUDm_USO9QldUziNuq3J6iV2HjLLb-70ztCbhnMGKj0Qc4AJAclzsiEScmSTDF1TiYAhUi4SD8uyVXfbwB4kWX5hPilp3FtKXbR1a5y2NAB95YGrL5spMbubdOGrfWROk-R9gH94HpLt63ZNRitoWW78wa7A23wYDvaHgP7wYZIB-c_KUb6jtWa8pm8Jhc1Nr29OemUrJ6fVvPXZLF8eZs_LpLAIRUJq02dC5XlXFUlN1YVknHGWJFiLqDKihLACoUCapBKFSbH0mKWFxYqYyCdkrtjbOja753to960u86PjZrLlAkG443U_ZHqKxcxutbr0Lnt-Iret52W-jSlDqb-D2agf7f_M6Q_5el1IQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype><pqid>2531410000</pqid></control><display><type>conference_proceeding</type><title>On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2.5</title><source>AIP Journals Complete</source><creator>Panina, A. ; Yatskikh, A. ; Kosinov, A. ; Yermolaev, Yu ; Semionov, N.</creator><contributor>Fomin, Vasily ; Shiplyuk, Alexander</contributor><creatorcontrib>Panina, A. ; Yatskikh, A. ; Kosinov, A. ; Yermolaev, Yu ; Semionov, N. ; Fomin, Vasily ; Shiplyuk, Alexander</creatorcontrib><description>The results of an experimental study of the perturbation development created by pulsed glow discharge on the swept wing surface with periodic distributed roughness along the leading edge at Mach 2.5 are presented. This work continues research on this model at Mach 2. It was found that the mean flow modulation in the boundary layer of a swept wing with a sweep angle of 40 degrees leads to a change in the amplitude of artificial pulsations excited in the boundary layer by a disturbance source and to a strengthening of the oblique breakdown mechanism at a Mach number of 2.5.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0052064</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Boundary layers ; Glow discharges ; Mach number ; Perturbation ; Sweep angle ; Swept wings ; Wave packets</subject><ispartof>AIP conference proceedings, 2021, Vol.2351 (1)</ispartof><rights>Author(s)</rights><rights>2021 Author(s). Published by AIP Publishing.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://pubs.aip.org/acp/article-lookup/doi/10.1063/5.0052064$$EHTML$$P50$$Gscitation$$H</linktohtml><link.rule.ids>309,310,314,776,780,785,786,790,4498,23909,23910,25118,27901,27902,76126</link.rule.ids></links><search><contributor>Fomin, Vasily</contributor><contributor>Shiplyuk, Alexander</contributor><creatorcontrib>Panina, A.</creatorcontrib><creatorcontrib>Yatskikh, A.</creatorcontrib><creatorcontrib>Kosinov, A.</creatorcontrib><creatorcontrib>Yermolaev, Yu</creatorcontrib><creatorcontrib>Semionov, N.</creatorcontrib><title>On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2.5</title><title>AIP conference proceedings</title><description>The results of an experimental study of the perturbation development created by pulsed glow discharge on the swept wing surface with periodic distributed roughness along the leading edge at Mach 2.5 are presented. This work continues research on this model at Mach 2. It was found that the mean flow modulation in the boundary layer of a swept wing with a sweep angle of 40 degrees leads to a change in the amplitude of artificial pulsations excited in the boundary layer by a disturbance source and to a strengthening of the oblique breakdown mechanism at a Mach number of 2.5.</description><subject>Boundary layers</subject><subject>Glow discharges</subject><subject>Mach number</subject><subject>Perturbation</subject><subject>Sweep angle</subject><subject>Swept wings</subject><subject>Wave packets</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2021</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp9kD9PwzAUxC0EEqUw8A0ssSGlPDu2k4yo4p9U1KUDm_USO9QldUziNuq3J6iV2HjLLb-70ztCbhnMGKj0Qc4AJAclzsiEScmSTDF1TiYAhUi4SD8uyVXfbwB4kWX5hPilp3FtKXbR1a5y2NAB95YGrL5spMbubdOGrfWROk-R9gH94HpLt63ZNRitoWW78wa7A23wYDvaHgP7wYZIB-c_KUb6jtWa8pm8Jhc1Nr29OemUrJ6fVvPXZLF8eZs_LpLAIRUJq02dC5XlXFUlN1YVknHGWJFiLqDKihLACoUCapBKFSbH0mKWFxYqYyCdkrtjbOja753to960u86PjZrLlAkG443U_ZHqKxcxutbr0Lnt-Iret52W-jSlDqb-D2agf7f_M6Q_5el1IQ</recordid><startdate>20210524</startdate><enddate>20210524</enddate><creator>Panina, A.</creator><creator>Yatskikh, A.</creator><creator>Kosinov, A.</creator><creator>Yermolaev, Yu</creator><creator>Semionov, N.</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20210524</creationdate><title>On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2.5</title><author>Panina, A. ; Yatskikh, A. ; Kosinov, A. ; Yermolaev, Yu ; Semionov, N.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p2034-1fdf8467826cb2de6951211193a840c79b00e46a40f05669d8abea789e0cdd03</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Boundary layers</topic><topic>Glow discharges</topic><topic>Mach number</topic><topic>Perturbation</topic><topic>Sweep angle</topic><topic>Swept wings</topic><topic>Wave packets</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Panina, A.</creatorcontrib><creatorcontrib>Yatskikh, A.</creatorcontrib><creatorcontrib>Kosinov, A.</creatorcontrib><creatorcontrib>Yermolaev, Yu</creatorcontrib><creatorcontrib>Semionov, N.</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Panina, A.</au><au>Yatskikh, A.</au><au>Kosinov, A.</au><au>Yermolaev, Yu</au><au>Semionov, N.</au><au>Fomin, Vasily</au><au>Shiplyuk, Alexander</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2.5</atitle><btitle>AIP conference proceedings</btitle><date>2021-05-24</date><risdate>2021</risdate><volume>2351</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>The results of an experimental study of the perturbation development created by pulsed glow discharge on the swept wing surface with periodic distributed roughness along the leading edge at Mach 2.5 are presented. This work continues research on this model at Mach 2. It was found that the mean flow modulation in the boundary layer of a swept wing with a sweep angle of 40 degrees leads to a change in the amplitude of artificial pulsations excited in the boundary layer by a disturbance source and to a strengthening of the oblique breakdown mechanism at a Mach number of 2.5.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0052064</doi><tpages>4</tpages><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0094-243X |
| ispartof | AIP conference proceedings, 2021, Vol.2351 (1) |
| issn | 0094-243X 1551-7616 |
| language | eng |
| recordid | cdi_proquest_journals_2531410000 |
| source | AIP Journals Complete |
| subjects | Boundary layers Glow discharges Mach number Perturbation Sweep angle Swept wings Wave packets |
| title | On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2.5 |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-10T00%3A22%3A17IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_scita&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=On%20the%20artificial%20wave%20packet%20development%20in%20a%20spanwise%20modulated%20boundary%20layer%20on%20the%20swept%20wing%20at%20Mach%202.5&rft.btitle=AIP%20conference%20proceedings&rft.au=Panina,%20A.&rft.date=2021-05-24&rft.volume=2351&rft.issue=1&rft.issn=0094-243X&rft.eissn=1551-7616&rft.coden=APCPCS&rft_id=info:doi/10.1063/5.0052064&rft_dat=%3Cproquest_scita%3E2531410000%3C/proquest_scita%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2531410000&rft_id=info:pmid/&rfr_iscdi=true |