Access the full text.
Sign up today, get DeepDyve free for 14 days.
John Jackson (2020)
Classical ElectrodynamicsNature, 224
K. Sankaran, E. Choueiri, S. Jardin (2000)
Application of a New Numerical Solver to the Simulation of MPD Flows
O. Friedrich (1998)
Weighted Essentially Non-Oscillatory Schemes for the Interpolation of Mean Values on Unstructured GridsJournal of Computational Physics, 144
F. Cap (1994)
Lehrbuch der Plasmaphysik und Magnetohydrodynamik
H. Hügel
Zur Funktionsweise der Anode im Eigenfeldbeschleuniger
K. Fujita (1996)
Performance computation of a low-power hydrogen arcjet
C. Boie
Numerische Simulation magnetoplasmadynamischer Eigenfeldtriebwerke mit hochauflösenden adaptiven Verfahren
P.J. Turchi, P.G. Mikellides, K.W. Hohman, R.J. Leiweke, I.G. Mikellides, C.S. Schmahl, N.F. Roderick, R.E. Jr Peterkin
Progress in modeling plasma thrusters and related plasma flows
H. Minakuchi (1984)
Magnetoplasmadynamic Analysis of Plasma Acceleration
R. Jahn, F. Lyman (1968)
Physics of Electric Propulsion
M. Auweter‐Kurtz
Lichtbogenantriebe für Weltraumaufgaben
M. Auweter‐Kurtz, C. Boie, H. Habiger, H.J. Kaeppeler, H.L. Kurtz, P.C. Sleziona, T. Wegmann, M.W. Winter
Numerische Simulation von MPD–Triebwerken und Vergleich mit durchzuführenden experimentellen Untersuchungen
K.D. Goodfellow
A theoretical and experimental investigation of cathode processes in electric thrusters
U. Iben, G. Warnecke, J. Heiermann, M. Auweter‐Kurtz
Adaptive numerics for the simulation of magneto‐plasmadynamic rocket thrusters
J. Heiermann, M. Auweter‐Kurtz
Numerical simulation of high power steady state MPD thrusters
P.C. Sleziona
Hochenthalpiestro¨mungen fu¨r Raumfahrtanwendungen
G. Bennett, M. Watkins, D. Byers, J. Barnett (1990)
Enhancing Space Transportation: The NASA Program To Develop Electric Propulsion
M. Martínez-Sánchez (1991)
A two dimensional model of an MPD thruster
E. Choueiri (1999)
Anomalous resistivity and heating in current-driven plasma thrusters *Physics of Plasmas, 6
R. Devoto (1973)
Transport coefficients of ionized argonPhysics of Fluids, 16
For the numerical simulation of magnetoplasmadynamic (MPD) self‐field thruster flow, the solution of one of the two dynamical Maxwell equations – Faraday's law – is required. The Maxwell equations and Ohm's law for plasmas can be summarized in one equation for the stream function so that the two‐dimensional, axisymmetric magnetic field can be calculated. The finite volume (FV) discretization of the equation on unstructured, adaptive meshes is presented in detail and solutions for different thruster currents are shown. The calculated thrust is compared with the experimental data.
International Journal of Numerical Methods for Heat and Fluid Flow – Emerald Publishing
Published: Jun 1, 2004
Keywords: Plasma physics; Aerodynamics; Flow; Electromagnetic radiation
Read and print from thousands of top scholarly journals.
Already have an account? Log in
Bookmark this article. You can see your Bookmarks on your DeepDyve Library.
To save an article, log in first, or sign up for a DeepDyve account if you don’t already have one.
Copy and paste the desired citation format or use the link below to download a file formatted for EndNote
Access the full text.
Sign up today, get DeepDyve free for 14 days.
All DeepDyve websites use cookies to improve your online experience. They were placed on your computer when you launched this website. You can change your cookie settings through your browser.