This paper will present a validation of the turbulence modeling approaches used in the Helios code. Helios is a dual-mesh overset unstructured/Cartesian RANS solver developed by the US Army for high-fidelity simulation of rotorcraft aeromechanics. The paper will present validations of standard 3D flowfields using the current near-body unstructured code NSU3D as well as the new strand mesh solver that is intended to be adopted over the next few years.
Turbulent Flow Validation in the Helios Strand Solver
2014
27 pages
Report
Keine Angabe
Englisch
Turbulent Flow Validation in the Helios Strand Solver (AIAA 2014-0083)
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