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Experimental investigation on a cavity-step-actuated supersonic oscillating jet 被引量:2

Experimental investigation on a cavity-step-actuated supersonic oscillating jet
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摘要 Wind tunnel testing is conducted at different back pressures in a vacuum-type wind tunnel for a novel supersonic fluidic oscillator which consists of a two-dimensional Laval nozzle, a rectangular cavity and a backward step, to obtain its characteristics and the conditions for jet oscillating. The experimental results show that periodic asymmetrical flipping of the supersonic jet appears over certain nozzle pressure ratio(NPR) range according to schlieren visualization and pressure fluctuations. The jet flipping appears only when the jet is over expanded. The normalized average amplitude of the lateral pressure difference acting on the roofs of the cavity and the step varies around 0.2 while the periodic flipping appears. The supersonic jet periodic flipping frequencies obtained from the experiments agree well with those from the modified Rossiter mode for cavity-step acoustic resonance, but further investigations are needed to discover the underlying mechanism for the jet flipping. Wind tunnel testing is conducted at different back pressures in a vacuum-type wind tunnel for a novel supersonic fluidic oscillator which consists of a two-dimensional Laval nozzle, a rectangular cavity and a backward step, to obtain its characteristics and the conditions for jet oscillating. The experimental results show that periodic asymmetrical flipping of the supersonic jet appears over certain nozzle pressure ratio(NPR) range according to schlieren visualization and pressure fluctuations. The jet flipping appears only when the jet is over expanded. The normalized average amplitude of the lateral pressure difference acting on the roofs of the cavity and the step varies around 0.2 while the periodic flipping appears. The supersonic jet periodic flipping frequencies obtained from the experiments agree well with those from the modified Rossiter mode for cavity-step acoustic resonance, but further investigations are needed to discover the underlying mechanism for the jet flipping.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2017年第1期274-281,共8页 中国航空学报(英文版)
基金 supported by a grant from the Natural Science Foundation of Jiangsu Province (No. BK20150781)
关键词 Jet cavity interactions Jet flipping Oscillating jet Supersonic jet Wind runnel testing Jet cavity interactions Jet flipping Oscillating jet Supersonic jet Wind runnel testing
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  • 1Cattafesta LN, Sheplak M. Actuators for active flow control. Annu Rev Fluid Mech 2011;43:247-72.
  • 2Gregory W J, Tomac MN. A review of fluidic oscillator develop- ment and application for flow control. Reston: AIAA; 2013. Report No.: AIAA-2013-2474.
  • 3Raghu S. Fluidic oscillators for flow control. Exp Fluids 2013;54:1455.
  • 4Woszidlo R, Wygnanski IJ. Parameters governing separation control with sweeping jet actuators. Reston: AIAA; 2011. Report No.: AIAA-2011-3172.
  • 5Woszidlo R, Nawroth H, Raghu S, Wygnanski IJ. Parametric study of sweeping jet actuators for separation control. Reston: AIAA; 2010. Report No.: AIAA-2010-4247.
  • 6Phillips E, Woszidlo R, Wygnanski I. Separation control on a dynamic trailing-edge flap. Reston: AIAA; 2010. Report No.: AIAA-2010-4246.
  • 7Tewes P, Taubert L, Wygnanski IJ augment the lift of a lambda-wing No.: AIAA-2010-4689.
  • 8On the use of sweeping jets to Reston: AIAA; 2010. Report Seele R, Tewes P, Woszidlo R, McVeigh M, Lucas N, Wygnanski IJ. Discrete sweeping jets as tools for improving the performance of the V-22. J Aircraft 2009;46(6):2098-106.
  • 9Raman G, Raghu S, Bencic TJ. Cavity resonance suppression using miniature fluidic oscillators. Reston: AIAA; 1999. Report No.: AIAA-1999-1900.
  • 10Raman G, Packiarajan S, Papadopoulos G, Weissman C, Raghu S. Jet thrust vectoring using a miniature fluidic oscillator. Aeronaut J 2005;109(1093):12%38.

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