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Supersonic mixing enhanced by cavity-induced three-dimensional oscillatory flow

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Abstract

In this study, a novel wall-mounted cavity having a three-dimensional shape is proposed for enhancing supersonic mixing. This device induces an oscillatory secondary flow that effectively enhances mixing. To demonstrate the device performance, we experimentally compare supersonic mixing fields in three ducts without any devices, with a rectangular cavity, and with the newly proposed cavity (new device). In the experiments, time-dependent pressure measurements and oil-flow surface visualization are carried out. The experimental results show that the newly proposed cavity induces not only self-sustained flow oscillation but also secondary flow, both of which effectively enhance mixing. The jet issuing from the injector is also visualized for each duct by a planar laser-induced fluorescence (PLIF) technique. The PLIF visualizations reveal that mixing is enhanced far more rapidly in the duct with the newly proposed cavity than in the other ducts and that the jet penetration in the duct with the newly proposed cavity is much higher. These results are attributed to the large-amplitude jet fluctuation due to the oscillatory secondary flows induced by the newly proposed cavity.

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References

  • Cutler AD, Harding GC, Diskin GS (2013) High frequency pulsed injection into a supersonic duct flow. AIAA J 51:809–818

    Article  Google Scholar 

  • Gerlinger P, Stoll P, Kindler M, Schneider F, Aigner M (2008) Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced streamwise vorticity. Aerosp Sci Tech 12:159–168

    Article  MATH  Google Scholar 

  • Gruber MR, Nejad AS, Chen TH, Dutton JC (1996) Bow shock/jet interaction in compressible transverse injection flowfields. AIAA J 34:2191–2193

    Article  Google Scholar 

  • Gruber MR, Nejad AS, Chen TH, Dutton JC (1997) Compressibility effects in supersonic injection flowfields. Phys Fluids 9:1448–1461

    Article  Google Scholar 

  • Handa T, Masuda M, Kashitani M, Yamaguchi Y (2011) Measurement of number densities in supersonic flows using a method based on laser-induced acetone fluorescence. Exp Fluids 50:1685–1694

    Article  Google Scholar 

  • Handa T, Miyachi H, Kakuno H, Ozaki T (2012) Generation and propagation of pressure waves in supersonic deep-cavity flows. Exp Fluids 53:1855–1866

    Article  Google Scholar 

  • Heller HH, Holmes DG, Covert EE (1971) Flow-induced pressure oscillations in shallow cavities. J Sound Vib 18:545–553

    Article  Google Scholar 

  • Hynes AJ, Kenyon EA, Pounds AJ, Wine PH (1992) Temperature dependent absorption cross-sections for acetone and n-butanone—implications for atmospheric lifetimes. Spectrochim Acta 48:1235–1242

    Article  Google Scholar 

  • Lozano A, Yip B, Hanson RK (1992) Acetone: a tracer for concentration measurements in gaseous flows by planar laser-induced fluorescence. Exp Fluids 13:369–376

    Article  Google Scholar 

  • Nenmeni VA, Yu K (2002) Cavity-induced mixing enhancement in confined supersonic flows. AIAA Pap 2002−1010

  • Noren C, Vorobieff P, Truman CR, Madden TJ (2011) Mixing in a supersonic COIL laser: influence of trip jets. Exp Fluids 50:443–455

    Article  Google Scholar 

  • Papamoschou D, Hubbard DG (1993) Visual observations of supersonic transverse jets. Exp Fluids 14:468–476

    Article  Google Scholar 

  • Rana ZA, Thornber B, Drikakis D (2011) Transverse jet injection into a supersonic turbulent cross-flow. Phys Fluids 23:046103

    Article  Google Scholar 

  • Rogers RC, Capriotti DP, Guy RW (1998) Experimental supersonic combustion research at NASA Langley. AIAA Pap 98−2506

  • Rossiter JE (1964) Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds. ARC R&M 3438

  • Sato N, Imamura A, Shiba S, Takahashi S, Tsue M, Kano M (1999) Advanced mixing control in supersonic airstream with a wall-mounted cavity. J Prop Power 15:358–360

    Article  Google Scholar 

  • Seiner JM, Dash SM, Kenzakowski DC (2001) Historical survey on enhanced mixing in scramjet engines. J Prop Power 17:1273–1286

    Article  Google Scholar 

  • Thurber MC, Grisch F, Kirby BJ, Votsmeier M, Hanson RK (1998) Measurements and modeling of acetone laser-induced fluorescence with implications for temperature imaging diagnostics. Appl Opt 37:4963–4978

    Article  Google Scholar 

  • Yu KH, Schadow KC (1994) Cavity-actuated supersonic mixing and combustion control. Combust Flame 99:295–301

    Article  Google Scholar 

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Correspondence to Taro Handa.

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Handa, T., Nakano, A., Tanigawa, K. et al. Supersonic mixing enhanced by cavity-induced three-dimensional oscillatory flow. Exp Fluids 55, 1711 (2014). https://doi.org/10.1007/s00348-014-1711-y

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  • DOI: https://doi.org/10.1007/s00348-014-1711-y

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