Numerical analysis of the turbulent flow and alumina particle trajectories in solid rocket motors
Author:
Affiliation:
1. CIRA - Centro Italiano Ricerche Aerospaziali, Capua, Italy
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2860
Reference33 articles.
1. VORSTREM - A simple and versatile 2D viscous solver for chamber flow in solid rocket motors
2. A computational fluid dynamics analysis of the internal flow in a Titan SRMU
3. Deficiencies and requirements in modeling of slag generation in solid rocket motors
4. Modeling slag deposition in the Space Shuttle solid rocket motor
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