TY - GEN
T1 - Multicomponent simulation of plasma-sheath formation in presence of an emissive surface
AU - Gangemi, Giuseppe Matteo
AU - Hillewaert, Koen
AU - Magin, Thierry
AU - Alvarez Laguna, Alejandro
N1 - Publisher Copyright:
© 2024 by the American Institute of Aeronautics and Astronautics, Inc.
PY - 2024/1/1
Y1 - 2024/1/1
N2 - In a wall-confined environment, the plasma behaviour can be identified by dividing the domain in two main regions: the bulk, where the quasi-neutrality prevails (the charge density is close to zero) and the sheath region near the walls, where positive space charge is built. This phenomenon is due to a higher mobility of electrons, creating an electric potential structure that accelerates the ions towards the surface and repels the electrons. In this work we present a multicomponent approach to the problem of the formation of sheath in the presence of a thermionic emissive surface: this type of materials are of particular interest in the modeling of emissive probes or in novel thermal protection systems strategies that include the use of electron transpiration cooling materials for hypersonic leading edges.
AB - In a wall-confined environment, the plasma behaviour can be identified by dividing the domain in two main regions: the bulk, where the quasi-neutrality prevails (the charge density is close to zero) and the sheath region near the walls, where positive space charge is built. This phenomenon is due to a higher mobility of electrons, creating an electric potential structure that accelerates the ions towards the surface and repels the electrons. In this work we present a multicomponent approach to the problem of the formation of sheath in the presence of a thermionic emissive surface: this type of materials are of particular interest in the modeling of emissive probes or in novel thermal protection systems strategies that include the use of electron transpiration cooling materials for hypersonic leading edges.
U2 - 10.2514/6.2024-2605
DO - 10.2514/6.2024-2605
M3 - Conference contribution
AN - SCOPUS:85195965223
SN - 9781624107115
T3 - AIAA SciTech Forum and Exposition, 2024
BT - AIAA SciTech Forum and Exposition, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2024
Y2 - 8 January 2024 through 12 January 2024
ER -