2018
DOI: 10.1029/2018ja025743
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The Breakdown of the Fluid Approximation for Electrons in a Plasma Wake

Abstract: A comparative study using a fluid-based analytic solution, hybrid particle-ion fluid-electron particle-in-cell (PIC), and fully kinetic PIC is carried out to examine a collisionless, mesothermal plasma flow over a large, unbiased plate. We find that the plasma wake may be characterized into two regions based on the electron characteristics: a fluid electron expansion region and a kinetic electron expansion region. In the fluid electron expansion region, the electrons may be considered to be an equilibrium flui… Show more

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Cited by 14 publications
(6 citation statements)
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“…Hence, the proton flux collected by PSRs surface is that from a plasma wake. As the solar wind plasma expands into the wake, the ion velocity component normal to each expansion characteristic line equals to the ion acoustic speed (Wang & Hastings, 1992; Wang & Hu, 2018). For an order of magnitude estimation, we take the proton density above the lunar surface to be n ∼ 10 cm −3 and the proton impingement velocity to be the ion acoustic velocity Cs=Te/mi30 km/s.…”
Section: Formulation and Approachmentioning
confidence: 99%
“…Hence, the proton flux collected by PSRs surface is that from a plasma wake. As the solar wind plasma expands into the wake, the ion velocity component normal to each expansion characteristic line equals to the ion acoustic speed (Wang & Hastings, 1992; Wang & Hu, 2018). For an order of magnitude estimation, we take the proton density above the lunar surface to be n ∼ 10 cm −3 and the proton impingement velocity to be the ion acoustic velocity Cs=Te/mi30 km/s.…”
Section: Formulation and Approachmentioning
confidence: 99%
“…It is important to note that PSP is in a mesothermal plasma environment with plasma ion thermal velocities lower than the SW (∼300 km/s) and spacecraft speeds (up to 197 km/s), and plasma electron thermal velocities that remain greater than the spacecraft and solar wind velocities. A spacecraft in a mesothermal plasma forms a wake behind it (Ergun et al., 2010; Wang & Hastings, 1992; Wang & Hu, 2018). In addition to negative potential wake, for PSP an electrostatic barrier forms in the front of the spacecraft, as the ambient electrons penetrate the barrier while the photoelectrons and SE cannot (Ergun et al., 2010).…”
Section: Spacecraft Charging Overviewmentioning
confidence: 99%
“…[6][17]). However, the electron dynamics in wake regions have not yet been examined in detail [18]. In this study, we perform threedimensional electrostatic PIC simulations to examine a wake, considering in particular the plasma depletion region in the wake from the viewpoint of electron dynamics.…”
Section: Y Miyake Is With Education Center On Computational Science Andmentioning
confidence: 99%