HelixCS Parametric Finite Eleement Modeling

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.

FEM AI for future aerospace designs

HelixCS

Global Finite Element Modeling - Internal Load Models
2025
Technical Documentation

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.

FEM AIInternal LoadsGFEMVTOL
Parametric approach to Finite Element Modeling and Load development
2025
Technical Documentation

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.

FEM AICS-23Applied LoadsVTOL

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AI/ML-parametric finite element modeling for large aircraft and VTOL structures.

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