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Flow control of micro-ramps on supersonic forward-facing step flow 被引量:2

Flow control of micro-ramps on supersonic forward-facing step flow
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摘要 The effects of the micro-ramps on supersonic turbulent flow over a forward-facing step(FFS) was experimentally investigated in a supersonic low-noise wind tunnel at Mach number 3 using nano-tracer planar laser scattering(NPLS)and particle image velocimetry(PIV) techniques. High spatiotemporal resolution images and velocity fields of supersonic flow over the testing model were captured. The fine structures and their spatial evolutionary characteristics without and with the micro-ramps were revealed and compared. The large-scale structures generated by the micro-ramps can survive the downstream FFS flowfield. The micro-ramps control on the flow separation and the separation shock unsteadiness was investigated by PIV results. With the micro-ramps, the reduction in the range of the reversal flow zone in streamwise direction is 50% and the turbulence intensity is also reduced. Moreover, the reduction in the average separated region and in separation shock unsteadiness are 47% and 26%, respectively. The results indicate that the micro-ramps are effective in reducing the flow separation and the separation shock unsteadiness. The effects of the micro-ramps on supersonic turbulent flow over a forward-facing step(FFS) was experimentally investigated in a supersonic low-noise wind tunnel at Mach number 3 using nano-tracer planar laser scattering(NPLS)and particle image velocimetry(PIV) techniques. High spatiotemporal resolution images and velocity fields of supersonic flow over the testing model were captured. The fine structures and their spatial evolutionary characteristics without and with the micro-ramps were revealed and compared. The large-scale structures generated by the micro-ramps can survive the downstream FFS flowfield. The micro-ramps control on the flow separation and the separation shock unsteadiness was investigated by PIV results. With the micro-ramps, the reduction in the range of the reversal flow zone in streamwise direction is 50% and the turbulence intensity is also reduced. Moreover, the reduction in the average separated region and in separation shock unsteadiness are 47% and 26%, respectively. The results indicate that the micro-ramps are effective in reducing the flow separation and the separation shock unsteadiness.
出处 《Chinese Physics B》 SCIE EI CAS CSCD 2016年第5期233-237,共5页 中国物理B(英文版)
基金 Project supported by the National Natural Science Foundation of China(Grant Nos.11172326 and 11502280)
关键词 flow control micro-ramps separated flows flow imaging flow control micro-ramps separated flows flow imaging
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  • 1Gaitonde D V 2015 Prog. Aerospace Sci. 72 80.
  • 2Sun Q, Cui W, Li Y H, Cheng B Q, Jin D and Li J 2014 Chin. Phys. B 23 075210.
  • 3Li Q and Liu C Q 2010 J. Airerafi 47 2086.
  • 4Huang Y, Wang X N and Huang Z B 2013 Chin. Phys. Lett. 30 094702.
  • 5Frank K L, Li Q and Liu C Q 2012 Prog. Aerospace Sci. 53 30.
  • 6Lee S, Loth E, Georgiadis N J and DeBonis J R 2011 AIAA J. 49 97.
  • 7Anderson B H, Tinapple J and Suer L 2006 3rd A1AA Flow Control Conference, 5-8.June, San Francisco, USA, AIAA, p. 3197.
  • 8Babinsky H, Li Y and Ford C W P 2009 AIAA J. 47 668.
  • 9Blinde P L, Humble R A, van Oudheusden B W and Scarano F 2009 Shock Waves 19 507.
  • 10Sun Z, Schrijer F F J, Scarano F and van Oudheusden B W 2012 Phys. Fluids 24 055105.

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