Assessment of turbulence modeling for gas flow in two-dimensional convergent-divergent rocket nozzle

DOI10.1016/j.apm.2011.01.013zbMath1221.76137OpenAlexW2005646640MaRDI QIDQ638871

Juan-Miguel Gracia

Publication date: 16 September 2011

Published in: Applied Mathematical Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.apm.2011.01.013

zbMATH Keywords

shock wavecompressible flownumerical modelingturbulence modelsrocket nozzles

Mathematics Subject Classification ID

Finite volume methods for initial value and initial-boundary value problems involving PDEs (65M08)

Related Items

Numerical modeling for the combustion of simulated solid rocket motor propellant ⋮ A physically consistent and numerically robust \(k\)-\(\varepsilon\) model for computing turbulent flows with shock waves ⋮ Numerical modeling of turbulence-induced interfacial instability in two-phase flow with moving interface

Uses Software

• FLUENT
• STAR-CD

Cites Work

• A comparative study of turbulence models performance for separating flow in a planar asymmetric diffuser
• Experimental and numerical analysis of the structure of pseudo-shock systems in Laval nozzles with parallel side walls
• The numerical computation of turbulent flows
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