Gas density structure of supersonic flows impinged on by thin blades for laser-plasma accelerator targets

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Abstract

Density transition injection is an effective technique for controllably loading electrons into a trapped phase for laser plasma accelerators. One common technique to achieve the required fluid structure is to impinge a thin blade on the plume of a supersonic nozzle. Density transitions induced in this way are often assumed to be bow shocks and therefore sharp, but simulations and fluorescence measurements presented in this work show that in many cases of interest, the density transition accessible to a laser propagating transverse to the shock is an intercepting shock, and therefore, shock thickness and density vary with pressure, laser height, and blade position. The fluid dynamics of a supersonic nozzle impinged on by a thin, flat object are explored through simulations and relevant features are verified via planar laser-induced fluorescence measurements. The implications of the results for tuning electron beam injectors in laser plasma accelerators are discussed.

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Fan-Chiang, L., Mao, H. S., Tsai, H. E., Ostermayr, T., Swanson, K. K., Barber, S. K., … Leemans, W. P. (2020). Gas density structure of supersonic flows impinged on by thin blades for laser-plasma accelerator targets. Physics of Fluids, 32(6). https://doi.org/10.1063/5.0005888

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