Motion Model Dependencies in CFD-FASTRAN
Moving-body models
available in CFD-FASTRAN are highly suited to simulate complex prescribed and
six-degree-of-freedom (6DOF) motions of rigid bodies. In many engineering
problems, this translates to multiple bodies moving relative to one another.
Simulation of the Hypersonic Flow Past a Blunted Cone-cylinder-flare (HB-2) using CFD-FASTRAN
Study of supersonic flows is of high interest for a wide
variety of problems including design of high speed planes and other related
applications [1]. This user tip presents a validation of numerical methods
against experimental data.
Improvements to Parallel Simulation Setup in CFD-FASTRAN
Setting up and launching a parallel simulation has become much simpler and easier in FASTRAN. This note discusses some of these developments. Let’s start with things that have not changed. There are still two versions of CFD-FASTRAN solvers for parallel cases. The difference between the two versions is the underlying parallel communication mechanism, the choice of which is decided by the type of mesh used.
Improved Residual Plotter in CFD-FASTRAN-GUI
In V2006, the Residual Plotter in CFD-FASTRAN-GUI has
been improved to plot all of the output files that
CFD-FASTRAN creates. In addition to the global
residual history (RSL), CFD-FASTRAN may produce
output files with the extensions *.RZ, *.FORCE,
*.VFORCE, *.AFS, *.DYNA, *.DYNB, *.KINA, *.KINB,
depending on the problem.
Chemical-kinetic Model for Mars Atmosphere Re-entry Applications
The shock layer flow over a blunt body entering a
planetary atmosphere at a hypersonic speed will
dissociate and partially ionize. A reliable
prediction of the flow-field for such application
requires a chemical-kinetic model. For Mars
atmosphere, the five species Park'94 is considered
[1]. The dissociation of CO2 is producing C, CO, CO2,
O and O2.