Combustion Instability and Pressure Oscillation Numerical Simulation in a Solid Rocket Motor
Author:
Affiliation:
1. Italian Aerospace Research Center (CIRA)
2. Avio S.p.A.
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4952
Reference12 articles.
1. Simulations of Solid-Propellant Rockets: Effects of Aluminum Droplet Size Distribution
2. New insights into large eddy simulation
3. Numerical simulation of vortex shedding phenomenon in 2D test case solid rocket motors
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