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REACTIVE CONTROL OF...
REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER
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- Alarcón, José Faúndez (författare)
- KTH,Linné Flow Center, FLOW
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- Sasaki, Kenzo (författare)
- KTH,Linné Flow Center, FLOW
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- Hanifi, Ardeshir, Docent, 1963- (författare)
- KTH,Linné Flow Center, FLOW
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visa fler...
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- Larsson, Roger (författare)
- Saab Aeronautics, Bröderna Ugglas gata, SE-58188, Linköping, Sweden, Bröderna Ugglas gata
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- Henningson, Dan S. (författare)
- KTH,Linné Flow Center, FLOW
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visa färre...
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(creator_code:org_t)
- International Council of the Aeronautical Sciences, 2022
- 2022
- Engelska.
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Ingår i: 33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022. - : International Council of the Aeronautical Sciences. ; , s. 3037-3047
- Relaterad länk:
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https://urn.kb.se/re...
Abstract
Ämnesord
Stäng
- This investigation deals with the numerical implementation of a data-driven method for reactive control of the boundary-layer over a NACA0008 airfoil. The aim of this work is to evaluate the performance of controller in damping the flow disturbances and its efficiency in delaying laminar-turbulent transition. We focus our attention on the bypass transition scenario caused by free-stream turbulence. In this scenario, the perturbations in the wing boundary-layer develop into streaky structures. We show that this data-driven method is effective in decreasing the wall shear stress and disturbance energy at the objective location, and this damping is sustained downstream of the objective location. However, further downstream, the fluctuations grow again reaching amplitudes similar to those in the uncontrolled case.
Ämnesord
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)
Nyckelord
- Bypass transition
- Flow control
Publikations- och innehållstyp
- ref (ämneskategori)
- kon (ämneskategori)