CFD-FASTRAN solves the full Navier-Stokes equations
using a density-based finite- volume formulation and higher order differencing
schemes for the accurate prediction of subsonic, transonic or hypersonic
flows. The salient features of the solver include the following:
- Steady state and unsteady calculations
- Roe and Van-Leer upwinding flux functions
- Second and third order accurate schemes using the MUSCL approach with
Min-Mod, Osher-Chakravarthy and Van Leer limiters
- Multi-stage explicit Runge-Kutta, Point implicit and fully implicit
time integration schemes
- k-e, k-w*, Baldwin-Lomax,
Spalart-Allmaras and Menter-SST* turbulence models
- Supports multi-block structured, general unstructured (arbitrary type
elements) and chimera overset meshes
The CFD-FASTRAN flow solver has been extensively validated on numerous
benchmark problems and has been successfully used for many complex aerospace
applications. Please visit Aeromechanics
Applications for more information.
* Only available for structured meshes
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CFD-FASTRAN Flow Predictions
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