In-flight active wave cancelation with delayed-x-LMS control algorithm in a laminar boundary layer
This manuscript demonstrates the first successful application of the delayed-x-LMS (dxLMS) control algorithm for TS-wave cancelation. Active wave cancelation of two-dimensional broadband Tollmien–Schlichting (TS) disturbances is performed with a single DBD plasma actuator. The experiments are conduc...
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| Published in | Experiments in fluids Vol. 57; no. 10; pp. 1 - 16 |
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| Main Authors | , , , , , |
| Format | Journal Article |
| Language | English |
| Published |
Berlin/Heidelberg
Springer Berlin Heidelberg
01.10.2016
Springer Nature B.V |
| Subjects | |
| Online Access | Get full text |
| ISSN | 0723-4864 1432-1114 1432-1114 |
| DOI | 10.1007/s00348-016-2242-5 |
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| Abstract | This manuscript demonstrates the first successful application of the delayed-x-LMS (dxLMS) control algorithm for TS-wave cancelation. Active wave cancelation of two-dimensional broadband Tollmien–Schlichting (TS) disturbances is performed with a single DBD plasma actuator. The experiments are conducted in flight on the pressure side of a laminar flow wing glove, mounted on a manned glider. The stability properties of the controller are investigated in detail with experimental flight data, DNS and stability analysis of the boundary layer. Finally, a model-free approach for dxLMS operation is introduced to operate the controller as a ‘black-box’ system, which automatically adjusts the controller settings based on a group speed measurement of the disturbance wave packets. The modified dxLMS controller is operated without a model and is able to adapt to varying conditions that may occur during flight in atmosphere. |
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| AbstractList | This manuscript demonstrates the first successful application of the delayed-x-LMS (dxLMS) control algorithm for TS-wave cancelation. Active wave cancelation of two-dimensional broadband Tollmien–Schlichting (TS) disturbances is performed with a single DBD plasma actuator. The experiments are conducted in flight on the pressure side of a laminar flow wing glove, mounted on a manned glider. The stability properties of the controller are investigated in detail with experimental flight data, DNS and stability analysis of the boundary layer. Finally, a model-free approach for dxLMS operation is introduced to operate the controller as a ‘black-box’ system, which automatically adjusts the controller settings based on a group speed measurement of the disturbance wave packets. The modified dxLMS controller is operated without a model and is able to adapt to varying conditions that may occur during flight in atmosphere. |
| ArticleNumber | 160 |
| Author | Nemitz, Timotheus Grundmann, Sven Henningson, Dan S. Bagheri, Shervin Simon, Bernhard Fabbiane, Nicolò |
| Author_xml | – sequence: 1 givenname: Bernhard surname: Simon fullname: Simon, Bernhard email: simon@sla.tu-darmstadt.de organization: Institute for Fluid Mechanics and Aerodynamics, Technische Universität Darmstadt – sequence: 2 givenname: Nicolò surname: Fabbiane fullname: Fabbiane, Nicolò organization: Linné FLOW Centre, KTH Mechanics – sequence: 3 givenname: Timotheus surname: Nemitz fullname: Nemitz, Timotheus organization: Institute for Fluid Mechanics and Aerodynamics, Technische Universität Darmstadt – sequence: 4 givenname: Shervin surname: Bagheri fullname: Bagheri, Shervin organization: Linné FLOW Centre, KTH Mechanics – sequence: 5 givenname: Dan S. surname: Henningson fullname: Henningson, Dan S. organization: Linné FLOW Centre, KTH Mechanics – sequence: 6 givenname: Sven surname: Grundmann fullname: Grundmann, Sven organization: Department of Fluid Mechanics, University of Rostock |
| BackLink | https://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-195303$$DView record from Swedish Publication Index |
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| Cites_doi | 10.1016/S0142-727X(03)00051-1 10.1006/jsvi.1997.1484 10.1017/S0022112083002384 10.1260/1756-8250.7.1-2.37 10.1088/0022-3727/46/5/055202 10.1109/79.248551 10.1146/annurev.fluid.30.1.1 10.1115/1.4026604 10.1017/S0022112082001025 10.1016/0022-460X(90)90635-D 10.2514/3.49191 10.1017/jfm.2015.49 10.1007/s00348-007-0436-6 10.1017/jfm.2013.299 10.1063/1.863471 10.1017/S0022112082001037 10.1243/09544100JAERO540 10.1007/s00348-013-1610-7 10.2514/1.J051766 10.1017/S0022112008004394 10.1017/S0022112005008219 10.2514/1.J052485 10.1017/CBO9780511529535 10.1016/0021-9991(84)90128-1 10.1017/jfm.2015.45 10.1016/j.paerosci.2013.05.003 10.1016/j.ijheatfluidflow.2015.09.003 10.1146/annurev.fluid.34.082701.161921 10.1063/1.4817366 10.2514/1.J052141 10.1115/1.4033570 10.1201/9781482271461 10.2514/6.2014-1274 10.1007/978-3-319-27279-5_24 |
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| Snippet | This manuscript demonstrates the first successful application of the delayed-x-LMS (dxLMS) control algorithm for TS-wave cancelation. Active wave cancelation... |
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| SubjectTerms | Active control Actuators Algorithms Black boxes Boundary layers Broadband Control algorithms Control stability Control theory Controller setting Controllers Disturbance waves Disturbances Engineering Engineering Fluid Dynamics Engineering Thermodynamics Flight data Flow stability Fluid- and Aerodynamics Gliders Group speed Heat and Mass Transfer Laminar boundary layer Laminar flow Pressure side Research Article Stability Stability analysis Stability properties Wave packets Wing gloves |
| Title | In-flight active wave cancelation with delayed-x-LMS control algorithm in a laminar boundary layer |
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