Research on fluidic amplifiers dimensional modifications via computer simulation (CFD)
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Document typeConference report
Defense date2016
PublisherIstanbul Tecnical University
Rights accessRestricted access - publisher's policy
Abstract
When studying active flow control applications, it is already stated that activating the boundary layer via using periodic flow produces better performance than when employing steady blowing or sucking. This is why studying the performance characteristics of devices like fluidic oscillators and zero net mass flow actuators is particularly interesting. In the present paper a particular configuration of fluidic oscillator is carefully analyzed, initially its dynamic performance is compared with experimental results undertaken by previous researchers, then the dimensional internal characteristics are modified in order to obtain how is the dynamic behavior being affected, in a third stage the evaluation of how fluidic oscillators scale is affecting its dynamic performance is also presented. Based on the results obtained it can be concluded that a given actuator working at a given Reynolds number, is capable of producing different frequencies and amplitudes when modifying some dimensional parameters.
CitationBaghaei, M., Bergadà, J.M., Del Campo, D., Del Campo, V. Research on fluidic amplifiers dimensional modifications via computer simulation (CFD). A: International Conference on Computational Fluid Dynamics. "9th International Conference on Computational Fluid Dynamics, ICCFD9, Istanbul, Turkey, July 11-15, 2016: proceedings". Istanbul: Istanbul Tecnical University, 2016, p. 1-10.
Publisher versionhttp://iccfd9.itu.edu.tr/assets/pdf/papers/ICCFD9-2016-256.pdf
Collections
- Departament de Mecànica de Fluids - Ponències/Comunicacions de congressos [165]
- Departament de Física - Ponències/Comunicacions de congressos [563]
- L'AIRE - Laboratori Aeronàutic i Industrial de Recerca i Estudis - Ponències/Comunicacions de congressos [47]
- TUAREG - Turbulence and Aerodynamics in Mechanical and Aerospace Engineering Research Group - Ponències/Comunicacions de congressos [55]
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