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Morphology of shocked lateral outflows in colliding hydrodynamic flows

Supersonic interacting flows occurring in phenomena, such as protostellar jets, give rise to strong shocks and have been demonstrated in several laboratory experiments. To study such colliding flows, we use the AstroBEAR AMR code to conduct hydrodynamic simulations in three dimensions. We introduce...

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Published in:Physics of plasmas 2022-10, Vol.29 (10)
Main Authors: Markwick, R. N., Frank, A., Carroll-Nellenback, J., Blackman, E. G., Hartigan, P. M., Lebedev, S. V., Russell, D. R., Halliday, J. W. D., Suttle, L. G.
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container_issue 10
container_start_page
container_title Physics of plasmas
container_volume 29
creator Markwick, R. N.
Frank, A.
Carroll-Nellenback, J.
Blackman, E. G.
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Lebedev, S. V.
Russell, D. R.
Halliday, J. W. D.
Suttle, L. G.
description Supersonic interacting flows occurring in phenomena, such as protostellar jets, give rise to strong shocks and have been demonstrated in several laboratory experiments. To study such colliding flows, we use the AstroBEAR AMR code to conduct hydrodynamic simulations in three dimensions. We introduce variations in the flow parameters of density, velocity, and cross-sectional radius of the colliding flows in order to study the propagation and conical shape of the bow shock formed by collisions between two, not necessarily symmetric, hypersonic flows. We find that the motion of the interaction region is driven by imbalances in ram pressure between the two flows, while the conical structure of the bow shock is a result of shocked lateral outflows being deflected from the horizontal when the flows are of differing cross sections.
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source American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list); AIP_美国物理联合会现刊(与NSTL共建)
subjects Conical bodies
Conical flow
Cross-sections
Hypersonic flow
Outflow
Plasma physics
Protostars
Ram pressure
title Morphology of shocked lateral outflows in colliding hydrodynamic flows
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