Characteristics of unsteady type IV shock/shock interaction |
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Authors: | Email author" target="_blank">Y-B?ChuEmail author X-Y?Lu |
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Institution: | (1) Department of Modern Mechanics, University of Science and Technology of China, Hefei, 230026, Anhui, China |
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Abstract: | Characteristics of the unsteady type IV shock/shock interaction of hypersonic blunt body flows are investigated by solving
the Navier–Stokes equations with high-order numerical methods. The intrinsic relations of flow structures to shear, compression,
and heating processes are studied and the physical mechanisms of the unsteady flow evolution are revealed. It is found that
the instantaneous surface-heating peak is caused by the fluid in the “hot spot” generated by an oscillating and deforming
jet bow shock (JBS) just ahead of the body surface. The features of local shock/boundary layer interaction and vortex/boundary
layer interaction are clarified. Based on the analysis of flow evolution, it is identified that the upstream-propagating compression
waves are associated with the interaction of the JBS and the shear layers formed by a supersonic impinging jet, and then the
interaction of the freestream bow shocks and the compression waves results in entropy and vortical waves propagating to the
body surface. Further, the feedback mechanism of the inherent unsteadiness of the flow field is revealed to be related to
the impinging jet. A feedback model is proposed to reliably predict the dominant frequency of flow evolution. The results
obtained in this study provide physical insight into the understanding of the mechanisms relevant to this complex flow. |
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