Stability Analysis of Solid Rocket Motor Combustion by Computational Fluid Dynamics
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Kanagawa 229-8510, Japan
2. Tokai University, Kanagawa 259-1292, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.31976
Reference32 articles.
1. Longitudinal mode acoustic losses in short nozzles
2. Triggering axial instabilities in solid rockets - Numerical predictions
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