Assessment of Bhatnagar-Gross-Krook Approaches for Near Continuum Regime Nozzle Flows
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050208
Reference33 articles.
1. Examination of a Collision-Limiter Direct Simulation Monte Carlo Method for Micropropulsion Applications
2. The Space Environment and Its Effects on Space Systems
3. DSMC and Navier-Stokes Study of Backflow for Nozzle Plumes Expanding into Vacuum
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