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Tytuł artykułu

Influence of membrane amplitude and forcing frequency on synthetic jet velocity

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This paper presents the results of numerical investigations of a synthetic jet actuator for an active flow control system. The Moving-Deforming-Mesh method as a boundary condition is used to capture the real physical phenomenon. This approach allows precise investigation of the influence of the membrane amplitude, the forcing frequency and cavity effect on the jet velocity. A synthetic jet actuator is simulated using a membrane perpendicular to the surface arrangement. Two cases are investigated to maximize the jet velocity – an actuator with one and two membranes in a cavity. Two main forcing frequencies can be specified in the synthetic jet actuator application. One corresponds to the diaphragm natural frequency and the other corresponds to the cavity resonant frequency (the Helmholtz frequency). This study presents the results of actuators operating at the two abovementioned forcing frequencies. The simulation results show an increase in the jet velocity as a result of an increase in the membrane peak-topeak displacement. This study was a preliminary study of the synthetic jet actuator for single and double membrane systems. The optimization process of the synthetic jet actuator geometry and parameters is ongoing. Numerical results obtained in these investigations are to be validated in the experimental campaign.
Słowa kluczowe
Rocznik
Strony
111--120
Opis fizyczny
Bibliogr. 10 poz., rys., tab.
Twórcy
autor
  • Institute of Fluid-Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-952 Gdansk, Poland
autor
  • Institute of Fluid-Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-952 Gdansk, Poland
Bibliografia
  • [1] Casalino D, Diozzi F, Sannino R and Paonessa A 2008 Aerosp. Sci. Technol. 12 1
  • [2] Yen J and Ahmed N A 2013 J. Wind Eng. Ind. Aerodyn. 114 12
  • [3] Bechert D W, Meye R and Hage W 2000 Fluids 2000 conference and exhibit, Denver, CO, AIAA 2000
  • [4] Shan H, Jiang L, Liu C et al. 2008 Computers & Fluids 37 (8) 975
  • [5] Gul M, Uzol O and Akmandor I S 2014 J. Physics, Conference Series 524 1210
  • [6] Lee C Y and Goldstein D B 2002 AIAA J. 40 510
  • [7] Mallinson S G, Reizes J A and Hong G 2001 Aeronaut. J. 105 41
  • [8] Fugal S R, Smith B L and Spall R E 2005 Phys. Fluids 17 45103
  • [9] Menter F R 1994 AIAA J. 32 (8) 1598
  • [10] Gallas Q, Holman R, Nishida T, Carroll B, Sheplak M and Cattafesta L 2003 AIAA J. 41 (2) 240
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-21afd978-0720-4aed-b83e-f760cecae474
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