Development and Verification of Simplified Boundary Condition of SaOB Actuator

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000034" target="_blank" >RIV/00010669:_____/18:N0000034 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Development and Verification of Simplified Boundary Condition of SaOB Actuator
Original language description
CFD simulations of the AFC effect are usually highly time consuming and require extensive computational resources and effort. These aspects almost exclude the simulation of the actuator arrays and the application of AFC during the design process. This study is focused on the development of simplified surface boundary condition of the actuator's effect on the flow-field and to enable significant reduction of the computational resources. The simplified boundary condition is based on the high-fidelity unsteady CFD simulations of the internal flowfield of the Suction and Oscillatory Blowing (SaOB) actuator in still air condition and takes into account the time dependent flowfield variables at the actuator's exit. The developed boundary condition is applied to a dataset with flow control applied to a low-speed airfoil in cross flow to verify its effect on circulation.
Czech name
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Czech description
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Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
58th Israel Annual Conference on Aerospace Sciences, IACAS 2018
ISBN
9781510851399
ISSN
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e-ISSN
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Number of pages
12
Pages from-to
322-333
Publisher name
Israel Annual Conference on Aerospace Sciences
Place of publication
Neuveden
Event location
Tel-Aviv & Haifa
Event date
Mar 14, 2018
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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