Simcenter STAR-CCM+ Hypersonic rocket with exhaust nozzle engaged, using AutoCFL and Line Search Methods

2021-02-02T15:52:24.000-0500
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Summary

This is a reconfiguration of an older version of the same simulation file, using the new coupled solver features, including the Automatic CFL and Line Search Under-Relaxation Methods

Details

This is  rocket with the exhaust nozzle engine engaged flying at mach 25 free stream. No validation data, but it uses the most recent coupled solver functionality as the solver setup to maintain stability and robustness of the solution.



KB Article ID# KB000045398_EN_US

Contents

SummaryDetails

Associated Components

Design Manager Electronics Cooling In-Cylinder (STAR-ICE) Job Manager Simcenter STAR-CCM+