Tips & Tricks

Here you will find articles on how to solve specific issues related to ESI's software solutions. Missing ESI products will be added progressively. Each article has a short abstract which is accessible to everyone. As logged users you can see the full article with all attached screenshots, and you can post comments related to each article.

e-Café #2 PYFUN, PYSTOP - Programmer ses propres critères d'arrêt de calcul
Comment programmer des critères d'arrêt de calcul en Python
Jean-Charles Paulin
Virtual Performance
3

Static comfort – Different encrypted data display
How to display encrypted occupant when other data are also encrypted in the model.
Oriane Jammet-Reynal
Virtual Seat
55

Static Comfort - Sensors Grid
Sensors Grid Definition improvement in Virtual Seat Solution v2015 (VE 11)
Cécile Cabane
Virtual Seat
141

Trim Manufacturing – Trim Adviser
Trim Adviser improvement in Virtual Seat Solution v2015 (VE 11)
Cécile Cabane
Virtual Seat
142

CFD-FASTRAN/CFD-ACE+ coupling for thermal environment simulations
In certain applications, different regions of the computational domain experiences flow conditions that are so different that it is very difficult for a single solver to produce accurate results at the extremes. In many situations, such problems can be separated and...
Abraham Meganathan
CFD
41

Avoiding Chimera Errors in CFD-FASTRAN
This note discusses a common error encountered by users when trying chimera meshes in CFD-FASTRAN. Such errors are easy to avoid and hopefully this note will assist you.
Abraham Meganathan
CFD
5

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.
Abraham Meganathan
CFD
6

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).
Abraham Meganathan
CFD
6

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...
Abraham Meganathan
CFD
18

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...
Abraham Meganathan
CFD
29