The Use of Virtual Sub-cells in DSMC Analysis of Orbiter Aerodynamics at High Altitudes Upon Reentry
Author:
Affiliation:
1. NASA Johnson Space Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1030
Reference9 articles.
1. DSMC grid methodologies for computing low-density, hypersonic flows about reusable launch vehicles
2. Aerodymics of the Shuttle Orbiter at high altitudes
3. Rarefied-Flow Transition Regime Orbiter Aerodynamic Acceleration Flight Measurements
4. A parallel implementation of the direct simulation Monte Carlo method
5. Application highlights of the DSMC Analysis Code (DAC) software for simulating rarefied flows
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