INCA is a state-of-the-art flow code. It is valid for a wide range of compressible viscous flow fields, including transonic aircraft, hypersonic high altitude vehicles, automotive intakes/manifolds, and reacting combustors. The incompressible flow module extends the range of applicability to low speed flows.
INCA solves the complete compressible or incompressible Navier-Stokes equations using an advanced implicit finite-volume procedure on multi-block, body-fitted, computational grids. The flow domain can be divided into coupled grid blocks to simplify both the generation of the grid and the application of boundary conditions. A variety of flexible boundary-condition types, equation-of-state options, turbulence models and chemistry models makes INCA applicable to most flow fields of interest. A parallel-procesing version of INCA is also available.
Don Roberts
Vice President
Amtec Engineering, Inc.
PO Box 3633
Bellevue, WA 98009-3633
USA
206-827-3304
206-827-3989 (fax)
don@moclips.amtec.com
For applications in related solution areas, see the following indices: Aerodynamics, Aerospace, Automotive, Automotive Design, Combustion Analysis, Combustion Simulation, Compressor Design, Numerical Analysis, Parallel Processing, the developer index for Amtec Engineering, Inc. and the market segment index for Computational Fluid Dynamics (CFD).
