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Techniques for Modeling Torque Transfer between Concentric Cylindrical Components
Finite elements that use a piecewise linear approximation of geometry are perfectly adequate for modeling cylindrical components such as shafts and hubs in ...
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12th International LS-DYNA Conference
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Hail Impact Problem in Aeronautical Field
Crashworthiness is one of the aspects that must be taken into account till the design phase, especially in aeronautical field. Some bodies, impacting against ...
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10th European LS-DYNA Conference
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7 Simulation II - Impact-Cracks
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A data-driven methodology for the automated analysis and explanation of system behavior in crash simulations
Attributable to model size and complexity of numerical crash simulations, it is not feasible for the engineers to analyze each area or component in detail, ...
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14th European LS-DYNA Conference 2023
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Occupant Safety
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FEA Newsletter February 2011
NURBS-based Finite Elements in LS-DYNA from Stefan Hartmann, DYNAmore - May 23rd and 24th, 2011. The 8th European LS-DYNA Users Conference hosted by ALYOTECH ...
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FEA Newsletters
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FEA Newsletters 2011
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FEA Newsletter December 2003
Status of LS-DYNA version 970-971-980. JMAG showcased by JRI. Topcrunch.org: Web site for LS-DYNA Benchmarks.
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FEA Newsletters
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FEA Newsletters 2003
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FEA Newsletter June 2011
Articles: LS-PrePost Update, DatapointLabs Material Parameters for Crash/Safety CAE Simulation - Solutions: Cloud Service - Events: 12th International LS-DYNA ...
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FEA Newsletters
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FEA Newsletters 2011
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FEA Newsletter February 2007
SGI Altix performance on TopCrunch. LS-PrePost Online Dokumentation News Update
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FEA Newsletters
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FEA Newsletters 2007
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A Summary of the Space Shuttle Columbia Tragedy and the Use of LS-DYNA in the Accident Investigation and Return to Flight Efforts
On February 1, 2003, the Space Shuttle Columbia broke apart during reentry resulting in loss of 7 crewmembers and craft. For the next several months an ...
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8th International LS-DYNA Conference
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The Use of LS-DYNA in the Columbia Accident Investigation and Return to Flight Activities
During the launch of the Space Shuttle Columbia on January 16, 2003, foam originating from the external tank impacted the shuttle’s left wing 81 seconds after ...
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8th International LS-DYNA Conference
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Numerical Modelling of the Fluid Structure Interaction using ALE and SPH: The Hydrodynamic Ram Phenomenon
Vulnerability against high-velocity impact loads is a critical issue for the design of aerospace structures due to the fact that aircrafts can be subjected to ...
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11th European LS-DYNA Conference
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Impact and Failure