CORE
🇺🇦
make metadata, not war
Services
Services overview
Explore all CORE services
Access to raw data
API
Dataset
FastSync
Content discovery
Recommender
Discovery
OAI identifiers
OAI Resolver
Managing content
Dashboard
Bespoke contracts
Consultancy services
Support us
Support us
Membership
Sponsorship
Community governance
Advisory Board
Board of supporters
Research network
About
About us
Our mission
Team
Blog
FAQs
Contact us
Verification of an electron-carbon interaction model for DSMC schemes
Authors
M. Auweter-Kurtz
Franz Bozsak
G. Herdrich
D. Petkow
Publication date
28 June 2010
Publisher
'American Institute of Aeronautics and Astronautics (AIAA)'
Abstract
International audienceThe Direct Simulation Monte Carlo module of a fully kinetic 3D plasma particle code is currently under development at the Institute of Space Systems (IRS). As the complete discharge simulation of a non-stationary magnetoplasmadynamic thruster is intended, improved models for the DSMC (direct simulation monte carlo) based interaction evaluation in a highly rarefied and strongly disturbed plasma need to be used. For that purpose it is essential to avoid macroscopic quantities (like temperature) in the model approach. Therefore, a collision and reaction evaluation approach was developed and implemented which is based on energy dependent cross section data only. As the thruster propellant is Polytetrafluorethylen (PTFE) a large cross section data base was built, implemented, and verified based on the assumption of an initially fully dissociated and partially ionized plasma. The electron - heavy particle interactions of interest are elastic scattering (including polarization), collisional excitation, de-excitation, and recombination. In this work we present the model approach, details on the implemented Carbon related cross sections as well as the verification procedure which is based on the reproduction of rate coefficients in the range of 20.000 - 200.000 K. © 2010 by the authors
Similar works
Full text
Available Versions
HAL-Polytechnique
See this paper in CORE
Go to the repository landing page
Download from data provider
oai:HAL:hal-01025990v1
Last time updated on 12/11/2016