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.
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.
Axisymmetric 2D Convergent-Divergent Boattail Nozzle Simulation Using CFD-FASTRAN
The NASA D-1.22-L boattail nozzle configuration was
obtained from the MADIC (Multidisciplinary and Design Industrial Consortium)
program. The geometry definition and the flow conditions are documented in NASA
TP 1766 [1]. This user tip presents a validation of numerical methods against
experimental data.
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.
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.