Application of synthetic jets actuators in wing-pylon junction area to improve the high lift performances
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F16%3AN0000078" target="_blank" >RIV/00010669:_____/16:N0000078 - isvavai.cz</a>
Result on the web
<a href="https://www.eccomas2016.org/" target="_blank" >https://www.eccomas2016.org/</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Application of synthetic jets actuators in wing-pylon junction area to improve the high lift performances
Original language description
Synthetic jets actuators that produce a zero net mass flow rate have been locally applied at the pylon-wing junction to suppress the high-lift penalties caused by the closely coupled engine integration. The high fidelity numerical simulations utilizing unsteady Reyn-olds-averaged Navier-Stokes have been performed to simulate this problem. A wind tunnel model representing a 2,5D wing with pylon, nacelle and deployed high-lift devices is used for this study. Active flow control applied at the wing-pylon junction area can prevent the larger flow separation on the wing behind the nacelle caused by the slat cutback, increase the lift and to postpone the stall angle by interaction of the vortices from the SJA with vortices dominating this region. The performed unsteady CFD simulations demonstrate the possibility locally affect the flow by utilization of AFC. The geometrical setup of the actuators and the flow variables (blowing coefficient, actuation frequency) have been varied, as well. Two different shapes and positions of the nacelle's strike have also been considered during the simulations. The positive effect of the application of the SJA on maximum lift and stall angle has been observed .
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
<a href="/en/project/7E13056" target="_blank" >7E13056: 2nd Generation Active Wing – Active Flow- Loads & Noise control on next generation wing</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
ECCOMAS Congress 2016 - Proceedings of the 7th European Congress on Computational Methods in Applied Sciences and Engineering, Vol. 3
ISBN
978-618-82844-0-1
ISSN
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e-ISSN
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Number of pages
10
Pages from-to
6505-6514
Publisher name
National Technical University of Athens
Place of publication
Greece
Event location
Crete Island, Greece
Event date
Jun 5, 2016
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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