Direct Simulation Monte Carlo Analysis of Thruster Plumes/Satellite Base Region Interaction
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejon 305-701, Republic of Korea
2. Korea Aerospace Research Institute, Daejon 305-333, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.1975
Reference27 articles.
1. Modeling of a small hydrazine thruster plume in the transition flow regime
2. Experimental and numerical investigations of low-density nozzle and plume flows of nitrogen
3. Low-density nozzle flow by the direct simulation Monte Carlo and continuum methods
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