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A wide range of flow regimes can be simulated using STAR-CCM+, including inviscid, laminar, turbulent (RANS, LES, DES), transition modeling. incompressible through to hypersonic. Visualized here are the Mach contours on a Scud missile.
Streamlines on a trap wing : simulations were computed using the steady state, coupled flow solver with implicit integration and second order discretization and using the SST (Menter) k-ω turbulence model. This work was done as part of a drag prediction workshop.
Streamlines on a trap wing.
Temperature distribution on a gas turbine blade.
Thermal analysis and management
Thermal analysis and management
STAR-CCM+ Prediction of Mean Streamwise Velocity Component from Landing Gear
STAR-CCM+ Prediction of Mean Z-wise Vorticity from Landing Gear
Transient aeroacoustics simulation on landing gear.

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