AI and Parametric Finite Element Modeling for future Aerospace Engineering
HelixCS research spans to AI/ML using parametric FEM automation for development of advanced aerospace structures: Large Aircrafts, VTOL and Space Structures. Geometry with aerodynamics, meshing, load generation, analysis and sizing is driven by an AI/ML interactive tools and algorithms.
HelixCS
Global Finite Element Modeling - Internal Load Models
TENSOR Computational Sciences
HelixCS Technical Report TR-2021-04
VTOL Internal Load Models generated using Parametric Finite Element Modeling. Design loop driven by an AI/ ML & Parametric FEM.
Parametric approach to Finite Element Modeling and Load development
TENSOR Computational Sciences
HelixCS Technical Report TR-2023-04
A Parametric Finite Element Model generated in accordance with CS-23 flight envelope for multirotor VTOL configurations. Load updates are autonomous based on the sizing criteria and payloads.
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We collaborate with OEMs and academic institutions on structural analysis research. Reach out to discuss co-authorship, data sharing, or platform evaluation.
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