Cancellation of Tollmien–Schlichting Waves in Direct Vicinity of a Plasma Actuator
The active cancellation of Tollmien–Schlichting waves is a promising and energy-efficient laminar flow control technology with the goal of drag reduction by delaying laminar–turbulent transition. This paper analyzes, for the first time, the control mechanism in the direct vicinity of the actuator us...
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description | The active cancellation of Tollmien–Schlichting waves is a promising and energy-efficient laminar flow control technology with the goal of drag reduction by delaying laminar–turbulent transition. This paper analyzes, for the first time, the control mechanism in the direct vicinity of the actuator using particle image velocimetry. Artificial Tollmien–Schlichting waves are generated at a frequency of fTS=250 Hz in a two-dimensional zero-pressure-gradient flat-plate boundary layer (U∞=15 m/s). The Tollmien–Schlichting waves travel downstream and are attenuated with an unsteady dielectric-barrier-discharge plasma actuator force. Phase-locked particle image velocimetry measurements at an acquisition rate of facq=800 Hz in double-frame mode are conducted in the direct vicinity of the plasma actuator, resolving 16 phase angles of the wave cycle. The use of two cameras allows measurement of two full wavelengths of the Tollmien–Schlichting waves and a detailed analysis of the cancellation process. The phase-averaged velocity fields of the artificially generated Tollmien–Schlichting waves are validated with a linear stability theory. The wavelength, amplification, and shape of the Tollmien–Schlichting wave disturbances and the counterwaves generated by the plasma actuator are analyzed. |
doi_str_mv | 10.2514/1.J056265 |
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This paper analyzes, for the first time, the control mechanism in the direct vicinity of the actuator using particle image velocimetry. Artificial Tollmien–Schlichting waves are generated at a frequency of fTS=250 Hz in a two-dimensional zero-pressure-gradient flat-plate boundary layer (U∞=15 m/s). The Tollmien–Schlichting waves travel downstream and are attenuated with an unsteady dielectric-barrier-discharge plasma actuator force. Phase-locked particle image velocimetry measurements at an acquisition rate of facq=800 Hz in double-frame mode are conducted in the direct vicinity of the plasma actuator, resolving 16 phase angles of the wave cycle. The use of two cameras allows measurement of two full wavelengths of the Tollmien–Schlichting waves and a detailed analysis of the cancellation process. The phase-averaged velocity fields of the artificially generated Tollmien–Schlichting waves are validated with a linear stability theory. The wavelength, amplification, and shape of the Tollmien–Schlichting wave disturbances and the counterwaves generated by the plasma actuator are analyzed.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J056265</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Boundary layer control ; Cameras ; Cancellation ; Drag reduction ; Energy efficiency ; Flow control ; Fluid dynamics ; Image acquisition ; Laminar boundary layer ; Laminar flow ; Particle image velocimetry ; Plasma ; Plasma actuators ; Two dimensional boundary layer ; Velocity distribution ; Velocity measurement ; Wavelengths</subject><ispartof>AIAA journal, 2018-05, Vol.56 (5), p.1760-1769</ispartof><rights>Copyright © 2018 by Bernhard Simon. 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 ; employ the ISSN (print) or (online) to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2018 by Bernhard Simon. 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 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a328t-f988ce4a176e021bb153f933d6de730fb49dad02c58477f873a664b83a5f0ec23</citedby><cites>FETCH-LOGICAL-a328t-f988ce4a176e021bb153f933d6de730fb49dad02c58477f873a664b83a5f0ec23</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,777,781,27905,27906</link.rule.ids></links><search><creatorcontrib>Simon, Bernhard</creatorcontrib><creatorcontrib>Markus, Daniel</creatorcontrib><creatorcontrib>Tropea, Cameron</creatorcontrib><creatorcontrib>Grundmann, Sven</creatorcontrib><title>Cancellation of Tollmien–Schlichting Waves in Direct Vicinity of a Plasma Actuator</title><title>AIAA journal</title><description>The active cancellation of Tollmien–Schlichting waves is a promising and energy-efficient laminar flow control technology with the goal of drag reduction by delaying laminar–turbulent transition. This paper analyzes, for the first time, the control mechanism in the direct vicinity of the actuator using particle image velocimetry. Artificial Tollmien–Schlichting waves are generated at a frequency of fTS=250 Hz in a two-dimensional zero-pressure-gradient flat-plate boundary layer (U∞=15 m/s). The Tollmien–Schlichting waves travel downstream and are attenuated with an unsteady dielectric-barrier-discharge plasma actuator force. Phase-locked particle image velocimetry measurements at an acquisition rate of facq=800 Hz in double-frame mode are conducted in the direct vicinity of the plasma actuator, resolving 16 phase angles of the wave cycle. The use of two cameras allows measurement of two full wavelengths of the Tollmien–Schlichting waves and a detailed analysis of the cancellation process. The phase-averaged velocity fields of the artificially generated Tollmien–Schlichting waves are validated with a linear stability theory. The wavelength, amplification, and shape of the Tollmien–Schlichting wave disturbances and the counterwaves generated by the plasma actuator are analyzed.</description><subject>Boundary layer control</subject><subject>Cameras</subject><subject>Cancellation</subject><subject>Drag reduction</subject><subject>Energy efficiency</subject><subject>Flow control</subject><subject>Fluid dynamics</subject><subject>Image acquisition</subject><subject>Laminar boundary layer</subject><subject>Laminar flow</subject><subject>Particle image velocimetry</subject><subject>Plasma</subject><subject>Plasma actuators</subject><subject>Two dimensional boundary layer</subject><subject>Velocity distribution</subject><subject>Velocity measurement</subject><subject>Wavelengths</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><recordid>eNplkMtKAzEYhYMoWKsL3yAgCC6m5jLJpMtS7xQUrJdd-CeT2JTpTE1SoTvfwTf0SZxSwYWrnwPfOefnIHRMyYAJmp_TwR0Rkkmxg3pUcJ5xJV53UY8QQjOaC7aPDmKcd4oVivbQdAyNsXUNybcNbh2etnW98Lb5_vx6NLPam1nyzRt-gQ8bsW_whQ_WJPzsjW98Wm8sgB9qiAvAI5NWkNpwiPYc1NEe_d4-erq6nI5vssn99e14NMmAM5UyN1TK2BxoIS1htCy7h92Q80pWtuDElfmwgoowI1ReFE4VHKTMS8VBOGIN4310ss1dhvZ9ZWPS83YVmq5SMyqLnBDFeEedbSkT2hiDdXoZ_ALCWlOiN6Npqn9H69jTLQse4C_tP_gDcRxqgA</recordid><startdate>20180501</startdate><enddate>20180501</enddate><creator>Simon, Bernhard</creator><creator>Markus, Daniel</creator><creator>Tropea, Cameron</creator><creator>Grundmann, Sven</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>20180501</creationdate><title>Cancellation of Tollmien–Schlichting Waves in Direct Vicinity of a Plasma Actuator</title><author>Simon, Bernhard ; Markus, Daniel ; Tropea, Cameron ; Grundmann, Sven</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a328t-f988ce4a176e021bb153f933d6de730fb49dad02c58477f873a664b83a5f0ec23</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Boundary layer control</topic><topic>Cameras</topic><topic>Cancellation</topic><topic>Drag reduction</topic><topic>Energy efficiency</topic><topic>Flow control</topic><topic>Fluid dynamics</topic><topic>Image acquisition</topic><topic>Laminar boundary layer</topic><topic>Laminar flow</topic><topic>Particle image velocimetry</topic><topic>Plasma</topic><topic>Plasma actuators</topic><topic>Two dimensional boundary layer</topic><topic>Velocity distribution</topic><topic>Velocity measurement</topic><topic>Wavelengths</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Simon, Bernhard</creatorcontrib><creatorcontrib>Markus, Daniel</creatorcontrib><creatorcontrib>Tropea, Cameron</creatorcontrib><creatorcontrib>Grundmann, Sven</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>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Simon, Bernhard</au><au>Markus, Daniel</au><au>Tropea, Cameron</au><au>Grundmann, Sven</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Cancellation of Tollmien–Schlichting Waves in Direct Vicinity of a Plasma Actuator</atitle><jtitle>AIAA journal</jtitle><date>2018-05-01</date><risdate>2018</risdate><volume>56</volume><issue>5</issue><spage>1760</spage><epage>1769</epage><pages>1760-1769</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>The active cancellation of Tollmien–Schlichting waves is a promising and energy-efficient laminar flow control technology with the goal of drag reduction by delaying laminar–turbulent transition. This paper analyzes, for the first time, the control mechanism in the direct vicinity of the actuator using particle image velocimetry. Artificial Tollmien–Schlichting waves are generated at a frequency of fTS=250 Hz in a two-dimensional zero-pressure-gradient flat-plate boundary layer (U∞=15 m/s). The Tollmien–Schlichting waves travel downstream and are attenuated with an unsteady dielectric-barrier-discharge plasma actuator force. Phase-locked particle image velocimetry measurements at an acquisition rate of facq=800 Hz in double-frame mode are conducted in the direct vicinity of the plasma actuator, resolving 16 phase angles of the wave cycle. The use of two cameras allows measurement of two full wavelengths of the Tollmien–Schlichting waves and a detailed analysis of the cancellation process. The phase-averaged velocity fields of the artificially generated Tollmien–Schlichting waves are validated with a linear stability theory. The wavelength, amplification, and shape of the Tollmien–Schlichting wave disturbances and the counterwaves generated by the plasma actuator are analyzed.</abstract><cop>Virginia</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.J056265</doi><tpages>10</tpages></addata></record> |
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subjects | Boundary layer control Cameras Cancellation Drag reduction Energy efficiency Flow control Fluid dynamics Image acquisition Laminar boundary layer Laminar flow Particle image velocimetry Plasma Plasma actuators Two dimensional boundary layer Velocity distribution Velocity measurement Wavelengths |
title | Cancellation of Tollmien–Schlichting Waves in Direct Vicinity of a Plasma Actuator |
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