ATD-F350
Model Description
The ATD-F350 is a Finite Element (FE) representation of the FAA Hybrid III 50M dummy hardware, which is designed for aviation safety testing.
The ATD-F350 is derived from the ATD-H350. Its optimised lumbar spine, pelvis and leg adjustments meet FAA requirements for emergency landing tests, enabling precise load and movement measurements.
Some characteristics of the ATD-F350 are:
- Prestressed chest and jacket
- Prestressed joint buffers
- Same handling as the H350
- Jacket geometry mapped using computer tomography
FE Pre-Processors
- GNS Generator4
- Beta CAE Systems ANSA
- ANSYS LS-PrePost
- Altair HyperMesh
- Oasys PRIMER
FE Solver
- ANSYS LS-DYNA®*
- ESI VPS Pam-Crash* (upon request)
- Dassault Systèmes ABAQUS®* (upon request)
* The trade names are the property of the owning companies.
ATD Model Features
- High accuracy owing to physics-based modeling techniques
- FE models available for industry standard explicit FE codes
- Commonality of modeling standards for all dummy models
- Uniform discretization, nomenclature and numbering systems
- Same scripts for pre and post processing
- Same session file and application procedures
- Full utilization of code-specific features of each solver
Advantages for Users
- Systematic title nomenclature refers to the assembly groups
- Prefix in each title description allows a fast adjustment to the nomenclature of the load case
- Numeration not overlapping the assembly groups
- Advantage in pre and post processing
- Allows selection of assembly parts and groups
- Each assembly group close defined for itself
- Definition regarding the master, e.g. contacts relate to the assembly group
TRIAL INSTALLATION
You can try this product free of charge for 30 days.
Got a question about this product? We’d love to hear from you!
Contact Person:
Christian Pieper
Telephone:
E-Mail:
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