Multi-Species Fluid Dynamics for Hypersonic Flight
USimHS is a unique computational fluid dynamics code used for applications involving fluid flows at high Mach numbers. With USimHS, users can accurately simulate multi-species and multi-temperature fluid dynamics in hypersonic plasma regimes.
USimHS can be used for the design of spacecraft shielding for atmospheric re-entry, or combined with USimHEDP to study radio communications devices at hypersonic speeds or arc plasma torches. As one of the only commercial tools available for modeling high-Mach flows, USimHS is the trusted solution for hypersonic fluid dynamics.
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USimHS Advantages
- Fluid Dynamics Code for Hypersonic Plasma Regimes
- Solves on Structured or Unstructured Meshes
- Advanced Algorithms for Multi-Species Fluid Dynamics
- Accelerated Reaction Chemistry
- Visualization in Multiple Dimensionalities
- High Performance Computing Capable
- Documented Accuracy
- Powerful Post-Processing
- Robust Documentation and Tutorials
- Superior Customer Support
USimHS Capabilities
- Euler Equations
- Ideal Magnetohydrodynamic Equations
- Ideal Gas Equation Of State
- Real Gas Equation Of State
- General Equation Of State
- Multi-Temperature Compressible Flow
- Turbulence Modeling
- Accelerated Navier-Stokes Equations
- Reaction Chemistry
- Ablation
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Applications for USimHS
Spacecraft Shielding
Aircraft Propulsion
Hypersonic Aircraft Design
Hypersonic Vehicle Communications