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Compressible, density-based, explicit time-marching CFD solver for aerospace applications, supporting unsteady RANS, LES, DES, transition models, structured/unstructured meshes,...
Compressible, density-based, explicit time-marching CFD solver for aerospace applications, supporting unsteady RANS, LES, DES, transition models, structured/unstructured meshes, mixing plane, frozen rotor, sliding mesh interfaces, conjugate heat transfer, and moving mesh. Highly scalable via MPI.
Platforms, integrations, and language support vary by plan and region. Confirm final requirements with the vendor.
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Compliance claims are normalized from current vendor documentation and independently reviewed by SOTA2.