Numerical modeling for the combustion of simulated solid rocket motor propellant

DOI10.1016/J.COMPFLUID.2013.10.029zbMath1390.80012OpenAlexW2084102099MaRDI QIDQ1643715

Y. Aharonov

Publication date: 19 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2013.10.029

zbMATH Keywords

level set methodmoving interfacesalternating-direction-implicit (ADI) solverAP/HTPBsandwich propellantsolid rocket propellants

Mathematics Subject Classification ID

Combustion (80A25)

Cites Work

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• Assessment of turbulence modeling for gas flow in two-dimensional convergent-divergent rocket nozzle
• Uniformly high order accurate essentially non-oscillatory schemes. III
• Efficient implementation of weighted ENO schemes
• An Implicit Factored Scheme for the Compressible Navier-Stokes Equations

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