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Networked Embedded Systems for Active Flow Control in Aircraft
Polytechnic Institute of Porto.
Critical Materials S.A..
Polytechnic Institute of Porto.
Technische Universität Darmstadt.
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2012 (English)Report (Refereed)
Abstract [en]

Abstract— Aerodynamic drag is known to be one of the factorscontributing more to increased aircraft fuelconsumption. Theprimary source of skin friction drag during flight is theboundary layer separation. This is the layer ofair movingsmoothly in the immediate vicinity of the aircraft. In this paperwe discuss a cyber-physical system approachable ofperforming an efficient suppression of the turbulent flow byusing a dense sensing deployment to detect the lowpressureregion and a similarly dense deployment of actuators tomanage the turbulent flow. With this concept, onlytheactuators in the vicinity of a separation layer are activated,minimizing power consumption and also the induced drag.

Place, publisher, year, edition, pages
2012.
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:mdh:diva-23835OAI: oai:DiVA.org:mdh-23835DiVA, id: diva2:682352
Note

Publised in proceedings of the 11th International Workshop on Real-Time Networks (RTN2012), July 10th, 2012, Pisa, Italy.

Available from: 2013-12-27 Created: 2013-12-19 Last updated: 2014-01-27Bibliographically approved

Open Access in DiVA

No full text in DiVA

Other links

http://www.cister.isep.ipp.pt/docs/networked+embedded+systems+for+active+flow+control+in+aircraft/709/attach.pdf

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Bate, Iain

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CiteExportLink to record
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Citation style
  • apa
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Output format
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