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Velocity and temperature fluctuations characterize the combustion of heterogeneous solid propellants. We show how to mimic these boundary conditions for realistic numerical simulation to reproduce the observed pressure oscillations.
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This page is a summary of: Boundary Conditions for Inhomogeneous Combustion Simulation in Solid Rocket Motors, AIAA Journal, March 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j062554.
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