The shock-vortex interaction patterns affected by vortex flow regime and vortex models

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We have used a third-order essentially non-oscillatory method to obtain numerical shadowgraphs for investigation of shock-vortex interaction patterns. To search different interaction patterns, we have tested two vortex models (the composite vortex model and the Taylor vortex model) and as many as 47 parametric data sets. By shock-vortex interaction, the impinging shock is deformed to a S-shape with leading and lagging parts of the shock. The vortex flow is locally accelerated by the leading shock and locally decelerated by the lagging shock, having a severely elongated vortex core with two vertices. When the leading shock escapes the vortex, implosion effect creates a high pressure in the vertex area where the flow had been most expanded. This compressed region spreads in time with two frontal waves, an induced expansion wave and an induced compression wave. They are subsonic waves when the shock-vortex interaction is weak but become supersonic waves for strong interactions. Under a intermediate interaction, however, an induced shock wave is first developed where flow speed is supersonic but is dissipated where the incoming flow is subsonic. We have identified three different interaction patterns that depend on the vortex flow regime characterized by the shock-vortex interaction.
Publisher
Springer
Issue Date
2009-08
Language
English
Article Type
Article
Keywords

EFFICIENT IMPLEMENTATION; CAPTURING SCHEMES; SOUND GENERATION; STARTING VORTEX; WAVE; REFLECTION

Citation

SHOCK WAVES, v.19, no.4, pp.349 - 360

ISSN
0938-1287
DOI
10.1007/s00193-009-0210-1
URI
http://hdl.handle.net/10203/17709
Appears in Collection
AE-Journal Papers(저널논문)
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