A parametric investigation of jet and vortex actuator

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

Özet

The Jet and Vortex Actuator (JaVA) is a zero -net-mass flux device for active flow control. In this numerical study, we present a parametric study of JaVA in quiescent water and obtain time-averaged flow and vorticity fields. We systematically investigate the effect of the governing parameters that affect on the JaVA -induced flow characteristics. Three jet Reynolds numbers are investigated in detail; ReJ = 68, 150 and 250 and for each jet-Reynolds number, four different wide-slot to plate width ratios are considered: gw = 0.0166, 0.0338, 0.066 and 0.10. In all cases, the scaled amplitude is kept at Sa = 0.15 and 0.30 so that a total of 24 different simulations are investigated. JaVA-induced flow types are classified in five groups: wall-jet, vertical-oblique jet, chaotic jet, weak jet and vortex mode. Based on the governing parameters (Sa, ReJ and gw) all these flow types have been identified the jet-momentums are calculated from phaseaveraged jet velocities obtained from numerical modeling results and compared to each other. It is found that generally the vortex mode transports the highest momentum flux followed by a chaotic jet.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıDynamics, Vibration and Control; Energy; Fluids Engineering; Micro and Nano Manufacturing
YayınlayanWeb Portal ASME (American Society of Mechanical Engineers)
ISBN (Elektronik)9780791845844
DOI'lar
Yayın durumuYayınlandı - 2014
EtkinlikASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis, ESDA 2014 - Copenhagen, Denmark
Süre: 25 Tem 201427 Tem 2014

Yayın serisi

AdıASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis, ESDA 2014
Hacim2

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???event.eventtypes.event.conference???ASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis, ESDA 2014
Ülke/BölgeDenmark
ŞehirCopenhagen
Periyot25/07/1427/07/14

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Publisher Copyright:
Copyright © 2014 by ASME.

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