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.
Low Mach Preconditioning and Dual Time Stepping in CFD-FASTRAN
Density-based schemes employing time-marching procedures available
in CFD-FASTRAN provide excellent stability and convergence characteristics for
high-speed compressible flows (typically M >0.5).
CFD-FASTRAN-GUI Scripting for Text-Based Model Setup
CFD-FASTRAN-GUI can now be operated via a Python
Script in Version 2006, like CFD-ACE-GUI. GUI
scripting (and the DTF command) are intended to be
used in place of the AT file, which has now been
eliminated. The AT file has been the root cause of a
lot of confusion and unexpected problems, because it
was impossible to keep the state of the AT file
consistent with the state of the GUI.
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.
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.